Fake and Film II

Posted on December 25 2009 at 08:43 PM

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Fake and Film I

Posted on December 25 2009 at 08:41 PM

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German Heavy AFVS

Posted on December 24 2009 at 07:45 PM

The Tiger was one of the German responses to the appearance of new Soviet tanks in 1941 and in particular of the T-34. At the time the German Army had no heavy tanks, except for a few experimental vehicles. However, once the new Russian tanks were encountered the German High Command realised the need for tanks more powerful than the existing Pz.Kpfw.IV. In consequence two new tanks were hurriedly developed. One was the 56 ton Tiger, whose design incorporated some features of one of the earlier experimental tanks but which was armed with a tank version of the 88mm anti-aircraft gun that had already proved highly effective as an anti-tank weapon. The other was a new medium tank which became the Panther, a 43 ton vehicle armed with a 70 calibre long, high velocity 75mm gun. The Panther began to be produced in January 1943 and, together with the Tiger, gave the German tank units a qualitative superiority over the Russian tank units. But both tanks were produced on a relatively small scale, the total production of the original Tiger I amounting to 1354 and that of the Panthers to 5976 (1.75). In consequence, there were not enough Panthers to reequip the Panzer divisions completely with them and the Tigers were generally held back in independent battalions.

Both tanks had the same general layout as Pz.Kpfw.IV and five-man crews but apart from having much more powerful armament and thicker armour they were much more advanced mechanically. As a result of its combination of characteristics the Panther came to be regarded as the best medium tank of the 1943-45 period while the second version of the Tiger became the most powerful tank to be used during the Second World War. Thus, Tiger II was armed with a higher performance 88mm gun which was 71 calibres long and which could pierce considerably thicker armour than the 122mm gun of the IS-2. It was also heavily armoured, its frontal hull armour being 150mm thick, although this contributed to its weight of 68 tons, which made it the heaviest tank used during the war. But the total production of Tiger II amounted to only 489 vehicles.

In the meantime, while the Tiger and the Panther were being developed, the existing German tanks were belatedly armed with more powerful guns. In particular, Pz.Kpfw.IV was armed in 1942 with more powerful 75mm guns, first 43 and then 48 calibres long, instead of the short barrelled gun of 24 calibres, which had been used in German tanks since the Grosstraktoren of 1929.

New designs and improved versions of the existing vehicles developed in response to the appearance of the T-34 and KV not only made German tanks more than a match for the Soviet tanks in terms of gun-power but also put them well ahead of British and US tanks.

Post-War Heavy Tank Abandoned

During the 1960s there was also a shift of emphasis from nuclear weapons back to conventional forces as a result of the onset of strategic parity between the United States and the Soviet Union. In view of this and the fact that the armoured forces of the United States and its allies continued to be numerically inferior to those of the Soviet Union, the US Army made a major effort to gain qualitative superiority by developing in collaboration with the German Army a 'revolutionary new tank', which was designated MBT-70 (2.5). However, the MBT-70 programme proved to be over-ambitious and was terminated in 1971 by the US Congress on grounds of excessive cost. In consequence, the US Army embarked in 1972 on the development of a more conventional tank, the XM-1.

The controversy surrounding the MBT-70 obscured a significant change that had taken place at the time in US Army policy in favour of a single type of battle tank. The MBT-70 embodied it and moves towards it had already resulted in the withdrawal from service in 1964 of US heavy tanks. The Soviet Army retained its heavy tanks for several more years and they formed part of the Soviet forces which invaded Czechoslovakia in 1968. But during the 1970s the Soviet Army also concentrated on a single type of battle tank, as did other armies.

A policy of concentration on a single type of battle tank was eminently sensible because no other tank could be superior to it and. therefore, could be justified if the tank on which development concentrated was already as good as it could be as a battle tank. Other types of tanks could always be designed, of course, for different, special roles but they were bound to be inferior, overall, to the more versatile battle tanks designed to defeat the widest possible range of battlefield targets, including enemy tanks.

An extreme example of tanks designed for such special roles were the infantry and cruiser tanks which the British Army employed right up to the end of the Second World War in spite of their serious deficiencies. However, in 1944 while British troops were still fighting in Normandy, their commander, General Montgomery, proposed the abolition of the division between infantry and cruiser tanks and the adoption instead of a single type of 'capital' tank. As it happens, the latter was eventually developed into a heavy gun tank, which was used in small numbers between 1955 and 1966. But in the meantime the policy of using a single type of battle tank was put into effect with the adoption as such of the Centurion tank in 1949.

The French Army decided even earlier than the British to concentrate on a single type of battle tank. In fact, such a tank began to be considered even before the war ended and was developed as part of the French Army's post-war re-equipment programme. However, its development did not proceed beyond a number of prototypes and was abandoned in the mid-1950s when the French Army turned its attention to another and lighter type of battle tank. The latter stemmed from an agreement reached in 1957 with Germany to produce a common 'European' tank although, eventually, each country adopted its own design. But the French AMX-30 and the German Leopard retained at least one feature in common in being less heavily armoured than other contemporary tanks such as the British Chieftain and, to a lesser extent, the US M60 tank. In this respect their design reflected the view, which had become widespread, that heavy armour was no longer as valuable as it had been because of progress in the development of anti-tank guided missiles and other weapons with shaped charge warheads that could perforate the thickest tank armour.

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THE K5 GUNS Part II

Posted on December 23 2009 at 05:57 AM

Also considerably more practical than 'Gustav' and 'Dora' were the K5 guns in 28cm calibre, which fired 255kg (5651b) shells out to a range of close to 64km (40 miles). A total of 28 of these were constructed between 1936 and 1945, and all were used most effectively in combat, the most famous probably being 'Anzio Annie', which was used to bombard the Anzio beachhead, and is now on display at the US Army's artillery proving grounds at Aberdeen, Maryland. Like the Paris Guns, the K5 employed deeply incised rifling - the 12 grooves were 7mm (0.25in) deep - and each shell had very precisely machined curved slots into which were inserted soft iron rails to form splines, matching the pattern in the barrel exactly, instead of the simple lugs or studs of the original. These guns too were mounted on railway cars, though unlike the 'Gustav Gerät', they were transportable largely intact, and could thus be put into and out of action much more quickly and easily. They were fully practical weapons, and the smaller 24cm K3, built by Rheinmetall, was perhaps better still, especially in its improved form, the Krupp-developed K4.

However, that did not prevent the development of projects to improve on these weapons. One of those was to produce a rocket-assisted projectile (RAP), which grew out of an attempt to develop a 15cm RAP for an existing gun. This proved to be much more practicable in the extra volume available. The shell was in two parts, the head containing the solid propellant, with a blast tube leading down to the base, surrounded by a conventional high-explosive filling. The propellant was ignited by a time fuze which detonated 19 seconds into the projectile's flight when it was approaching the apogee of its trajectory and boosted its velocity. The maximum range achieved on test was 86.5km (53.7 miles), and it was calculated that half the shells would land in an elongated target area around 3500m (11,482ft) long and 200m (656ft) wide, which was entirely acceptable given the nature of the likely targets.

The RAP, an accepted part of the artilleryman's arsenal only by the 1980s, was not the only new projectile developed for the K5 gun. Scientists at Pennemünde also became involved in the attempts to increase the K5's range, and came up with the Pfeilgeschoss, in this case a projectile 120mm (4.7in) in diameter, 1.8m (6ft) long, with four fins and a form of rudimentary sabot, which was little more than a three-part flange, 31cm (7.9in) in diameter, which was to be fired from a version of the gun with a smooth-bore barrel bored out to that same calibre. The sabot flange was discarded as soon as the projectile was in free flight. With a suitable propellant charge to take its trajectory well into the stratosphere, this projectile, which had a 25kg (551b) explosive payload, reached a maximum range of almost 155km (95 miles). Development began as early as 1940, but with a low-grade priority it did not culminate until 1944. Pfeilgeschossen were issued, and seem to have been used in combat, albeit in small numbers, in 1945. The projectile was the forerunner of the FSDS (fin-stabilised, discarding sabot) round, now in common use. The credit for the original idea is usually accorded to a French gun designer, Edgar Brandt, better known for the infantry mortars he developed; in the 1930s he produced a very effective 105mm/75mm projectile, which had very superior performance when fired from a 105mm gun with a standard charge.

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THE K5 GUNS Part I

Posted on December 23 2009 at 05:54 AM

28 CM KANONE 5 IN EISENBAHNLAFETTE (28 CM K 5 (E))

The K 5 became the standard Army railway gun. Design began in 1934, and weapons entered service in 1936. Designed as a super long- range weapon using deep-grooved barrels and splined projectiles, four types entered service. The K 5 Tiefzug 10 mm was the first, the barrel made with twelve 10 mm grooves. However, after a series of split barrels, the depth of the grooves was reduced to 7 mm - the result was the K 5 Tiefzug 7 mm. The K 5 Vz was also developed, and had a multi-grooved barrel. Finally, a version with a bored-out barrel was produced, designed to fire Peenemunde arrow shells. As well as the four versions of the K 5, thought was also given to extending the range, and to this end a rocket-assisted shell was issued, the propellant in the nose section ignited by a time fuse after 19 seconds in flight. In 1943, the Army expressed interest in a weapon which was capable of being deployed even when the rail track had been destroyed, and which would also be capable of being transported on the chassis and running gear of the Tiger tank. However, the project was still in the development stage when the war ended.

More commonly known as “Anzio Annie” from one example’s use against Allied forces in the 1944 invasion of Italy, the 283mm K5 (E) was also known to the Germans as “Leopold.” Entering service in 1940, it weighed 480,607 pounds and mounted a horizontal sliding block and 802-inch-long barrel. Firing a special 561-pound splined shell, it had a maximum range of nearly 39 miles. The Germans fielded some twenty-five K5 (E)s during World War II, with one survivor now held at Aberdeen Proving Ground in Maryland and another in France.

283mm K5 (E)

Adoption date: 1940

Caliber : 283mm

Weight : 480,607 pounds

Breech : horizontal sliding block

Barrel length: 802 inches

Elevation : 50°

Traversal : 1°

Projectile weight: 561 pounds

Ammunition: Separate-loading, cased charge

Muzzle velocity: 3,700 fps

Maximum range: 39 miles

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Czech and Polish T-34s

Posted on December 20 2009 at 10:53 PM

Polish T-34/76 Model 1943 in Poznań, Poland

Former Czechoslovakia

Tanks

  • T-34-85CZ - Czechoslovak production version of T-34-85 Model 1944 medium tank. It is also known under designation T-36.
  • T-34-85 modernized by Czechoslovakia for export. These were of Soviet production. Such tanks were sold to Syria.

Support vehicles

  • MT-34 (1950s) (MT stands for mostniy tank - bridging tank) - Czechoslovakian conversion with PM-34 scissors bridge carried on rollers on top of a turretless T-34.[1]
  • VT-34 (VT stands for vyprošťovací tank - recovery tank) - Czechoslovakian purpose-built recovery vehicle with a front vertical, flat-plate superstructure with a bow mounted machine gun and a radio antenna in the front on the right hand side, driver's vision slot and a searchlight in the front on the left hand side and two rectangular top hatches similar to those in Soviet BTR-50PK and Czechoslovak/Polish OT-62 TOPAS tracked APCs. The equipment included a winch with a capacity of 30 tonnes and large wide three-angle entrenching spade in the back with its top inset for winch rope at rear.[1]
  • JT-34 - T-34 fitted with a large crane on a rotatable mount fitted in the turret ring.

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Messerschmitt Me 163 Komet

Posted on December 20 2009 at 10:52 PM

The diminutive Me 163 Komet did not alter the war's history, but was an imaginative idea. Principal drawback to the concept was the dangerous fuel.

There can be little doubt that if the Messerschmitt Me 163 rocket-powered fighter had been available to the Luftwaffe in quantity a year earlier, the Allied daylight bombing programme would have proved even costlier than it was. With an extra year of development behind it, the Me 163's problems, particularly those concerned with handling its unstable mixture of rocket fuels, might well have been solved, but the whole programme was at the edge of a new technology range, and time was not on Germany's side.

Research had been proceeding in Germany into the possibility of rocket-powered aircraft since the 1920s and Dr Alexander Lippisch, who had been working on tailless sailplane designs, produced the DFS 194 glider in a basic layout which was to be developed into the Me 163. Lippisch and his team joined Messerschmitt in January 1939 and began work on adapting the DFS 194 airframe to take an 882-lb (400-kg) thrust Walter rocket motor. This motor had already flown in the experimental rocket-powered He 176, but that programme had been unsatisfactory. The DFS 194, on the other hand, reached a speed of 342 mph (550 km/h) during tests and this led to increased momentum in the programme, Messerschmitt receiving an order for six prototypes designated Me 163A.

The first prototype was tested originally as a glider, towed behind a Messerschmitt Bf 110, and its flying qualities were good, the few problems being easily ironed out. In the summer of 1941 two of the prototypes were taken to Peenemünde for powered trials with the new Walter HWK RII-203b rocket motor, which gave 1,653-lb (750-kg) thrust, and the Me 163 was soon attaining speeds of up to 550 mph (885 km/h). Since only a small amount of rocket fuel could be carried there was a danger of running out before higher speeds could be attained but on one occasion, after being towed to a height of 13,125 ft (4000 m), test pilot Heini Dittmar cast off, fired the engine and accelerated to reach the remarkable speed of 623.85 mph (1003.9 km/h) before suffering a loss of stability as a result of compressibility effects. This phenomenon was to become well known later as aircraft approached the speed of sound. Dittmar corrected the situation but a redesign of the wing was undertaken to combat this fault.

There was, in fact, more danger at this stage of the programme in the instability of the fuel, which was a mixture of 80 per cent hydrogen peroxide with oxyquinoline or phosphate (T-Stoff) and an aqueous solution of calcium permanganate (Z-Stoff). An imbalance of these fuels in the combustion chamber could cause an explosion and occasionally did; a replacement for Z-Stoff using a different catalyst (30 per cent hydrazine hydrate solution in methanol) was called C-Stoff and was developed for use in the Waiter RII-211 which, in its production form for the later Me 163B was the HWK 109-509A.

Since the Me 163 had to be as light as possible, in order to get the maximum performance from its very limited fuel load, the weight penalty of retractable landing gear was not acceptable. Thus, the take-off was made using a jettisonable two-wheel dolly, the aircraft landing on a retractable skid beneath the forward fuselage plus the tailwheel. The method caused problems, since take-offs had to be made directly into wind; if a concrete runway was to be used and there was a crosswind it was impossible to get airborne as the aircraft would not keep straight below the speed at which the rudder became operative. A subsequent modification to couple rudder control to rocket ignition partially cured this.

Following the six Me 163A prototypes, a preproduction series of 10 Me 163A-0 aircraft was built by Wolf Hirth, the sailplane company, and these were used as training gliders. However, considerable redesign took place before the operational Me 163B Komet (comet) flew. Six prototypes and 70 production models were ordered, but troubles with the new rocket motor held up the programme, and fuel consumption was almost double the calculated figure. Production was subcontracted to a number of component manufacturers and the parts were assembled in a Black Forest factory under the supervision of Klemm Technik GmbH, although this company had many problems since the sub-contractors were not accustomed to close-tolerance work.

First production deliveries of Me 163B-1a interceptors began in May 1944, and the type saw action for the first time on 28 July, when five Me 163s from l./JG 400, the first operational unit, ineffectively attacked a formation of Boeing B-17s near Merseburg. Their difficulties can be appreciated when it was realised that approaching the target at around 559 mph (900 km/h) when the bombers were travelling at 250 mph (402 km/h). The closing speed allowed the attacker only a three-second burst from a slow-firing cannon before he had to break away. Because of the poor results with the MK 108 cannon an alternative weapon had to be found.

One answer was certainly unusual; the SG 500 Jagdfaust consisted of five vertically mounted firing tubes in each wing root, each containing a 50-mm shell. The system fired in a salvo and was activated by the shadow of the target passing over a light cell (unfortunate if it happened to be your wingman) and the Me 163 merely had to fly at high speed beneath the bomber formation, when the armament was activated automatically. The Jagdfaust system was fitted to 12 Me 163Bs but, although these were not issued for operations, this unlikely weapon destroyed a B-17 on one occasion.

In 1944, to help convert the dwindling supply of pilots to the Me 163, a tandem trainer variant designated Me 163S was developed, an adaptation of the Me 163B with ammunition, T-Stoff tanks and other items removed to make way for the extra seat. The Me 163S was flown only as a glider and few were converted. Production of the Me 163B-1a ended in February 1945 after almost 400 of all variants had been built. Projected developments included the Me 163C and Me 163D; the former was a modification of the Me 163B with an auxiliary cruising chamber to improve endurance, a new centre-section and a more streamlined fuselage with a blister canopy. Three Me 163C-la aircraft were built, but only one was flown. The Me 163D was further refined and had retractable tricycle landing gear. One prototype was built and, since Junkers had been tasked with development and series production of this model, it was for a while known as the Ju 248 before reverting to a Messerschmitt designation as the Me 263. It did not enter production, the prototype being captured by the Russians who fitted it with new straight wings and modified tail surfaces, flying it in 1946 as the I-270(ZH), but it was soon abandoned.

Mention should be made of a licence-built version of the Me 163B, the Mitsubishi Ki-200 (J8M1), which was to be built in Japan with Mitsubishi and Yokosuka building the HWK 509A motor. Loss of the pattern aircraft on a ship en route to Japan left the Japanese with only an instruction manual, and it is to their credit that they began design of an airframe based on the Me 163B. The first aircraft flew in July 1945 but was destroyed when the motor failed. Several others were built but the programme was terminated by the end of the war.

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T-55

Posted on December 18 2009 at 04:45 AM

This Iraqi T-55 sports add-on armour on both turret and hull.

T-55AM2B with additional armour

The first postwar Soviet MBT, introduced in 1948, was the formidable T-54, itself a refinement of the T-44, the short-lived redesign of the T- 34/85 at the end of World War II. The T-54 had improved mechanical ability, especially in its torsion-bar suspension and transmission. It had five road wheels per side, with a noticeable gap between the first and second road wheels. There were no return rollers. The original turret design tended to deflect rounds downward into the turret ring and was replaced by a more hemispherical “frying pan” shape with internal mantlet.

The T-54 had a longer hull than the T-44, as well as a larger and better-shaped turret. It also had improved tracks, a torsion-bar suspension system, and a transverse-mount engine at the hull rear. The T-54 weighed some 79,300 pounds, had a crew of four, and a 520- hp diesel engine giving a maximum road speed of 30 mph. It mounted a 100mm main gun and three machine guns. The bow machine gun, done away with on the T-44, resurfaced in the T-54, but without return of the crewman for it; manning the bow gun was now the responsibility of the driver. The T-54 had maximum 203mm armor protection.

In the mid-1950s the T-54 received a bore evacuator near the muzzle of the main gun, which was also stabilized for elevation. The T-54B of 1957–1958 introduced a stabilized gun for both elevation and traverse. It also had infrared driving lights and snorkel equipment enabling it to cross rivers while submerged.

The T-55 appeared beginning in 1958. The chief difference between it and the T-54 was in the latter’s more powerful V-55 580-hp diesel engine. It also had a slightly modified turret, an improved 100mm main gun, a better transmission, a revolving turret floor (meaning that the crew did not have to shift position as the turret rotated), and increased ammunition storage. In 1963 the T-55 received an NBC system. The bow machine gun was also eliminated. In the late 1980s the T-55s received new supercharged engines, improved fire-control and laser-range finding systems, and appliqué and explosive armor.

The T-54/T-55 had a very long service life. Production continued until 1981, with a phenomenal 95,000 tanks manufactured, more than any other tank in history. Both the Chinese and Romanians have produced copies. Even at the end of the Cold War the T-54/T- 55 constituted some 38 percent of overall Soviet tank strength and as much as 86 percent of non-Soviet Warsaw Pact armor. Reliable and relatively inexpensive, the T-54/T-55 was exported to more than 35 other nations (outside of the Warsaw Pact these included Egypt, Finland, India, Iraq, Libya, and Syria). Although obsolescent, these tanks nonetheless remain in service today. Egypt has upgraded its T- 55s with U.S. engines, guns, and fire-control systems. Israel captured a number of T-54/T-55s from Egypt and Syria and proceeded to upgrade them with General Motors engines and 105mm M68 guns.

The T-54/T-55s have had a mixed combat record. Although sufficient to crush the Hungarian Revolution of 1956, they were not successful against Western-supplied Israeli armor in the 1967 Six Day War. They continued as the mainstay of Egyptian as well as Syrian armor in the 1973 Yom Kippur War, and although these tanks inflicted losses on Israeli tanks in that conflict, the Arab armies were again defeated. This was more a failure of doctrine and training than of equipment, however. The T-55 continued to serve in Africa, Asia, Afghanistan, and in Iraq. They were easily outclassed by the Coalition’s armor in the 1991 Gulf War.

Summary: A further development of the mechanically unreliable T-44, itself derived from the T-34. The chief difference between the T-54 and T-55 is a more powerful diesel engine. With the largest production run of any tank in history, the T-54/T-55, even at the end of the Cold War, constituted 38 percent of the Soviet tank inventory and about 85 percent of the non-Soviet Warsaw Pact inventory. The T-54/T-55 has been exported to more than 35 different nations, and although obsolescent today, it remains in widespread use.

Production dates: 1948–1981

Number produced: Approx. 95,000

Manufacturer: Soviet state factories

Crew: 4 (the bow gun reappeared but not the bow gunner; handling it is the responsibility of the driver)

Armament: 1 x 100mm main gun; 1 x 12.7mm DShK machine gun (antiaircraft); 2 x 7.62mm machine guns (bow, coaxial)

Weight: 79,344 lbs.

Length (excluding gun): 21’2”

Width: 10’9”

Height: 7’10”

Armor: maximum 203mm (steel)

Ammunition storage and type: 34 x 100mm; 500 x 12.7mm; 3,000 x 7.62mm

Power plant: V-2-5412-cylinder 520-hp diesel engine (T-54); V-55 580-hp diesel engine (T-55)

Maximum speed: 30 mph (T-54); 31 mph (T-55)

Range: 250 miles

Fording depth: 4’7”

Vertical obstacle: 2’7”

Trench crossing: 8’10”

Special characteristics (pos/neg): Can be equipped with snorkel device to allow submerged fording. Long-range fuel tanks extend mileage to 450 miles. T- 55A added infrared NBC system. In the late 1980s T-55s received new supercharged V-55U engines, improved fire control system, laser rangefinders, and appliqué and explosive armor.

Special models: many, including recovery vehicles; engineer vehicles; bridge-layers; mine-clearers

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THE MESSERSCHMITT P.1101, P.1110 AND P.1111

Posted on December 16 2009 at 06:34 PM

Another of the aircraft entered for the Emergency Fighter Competition was also to form the basis of a type built elsewhere, but this time rather more openly. The Messerschmitt company had in fact anticipated the need for a replacement for the Me 262 (who was in a better position to know that aircraft's limitations?) and construction of a prototype to replace it, designed by Woldemar Voigt, had begun in July 1944 as the P. 1101. This was in one particular a remarkable aircraft, for it was constructed chiefly to determine the best angle of wing sweep; its variable-chord wings could be reset (on the ground, not in flight) to any angle between 35 and 45 degrees. Otherwise, the aircraft was conventional in the new mould, with a single engine located deep within the fuselage and exhausting below the extension boom which supported the tail assembly.

The prototype was about 80 per cent complete when it was discovered by the Americans on their arrival in Oberammergau, and it was put on display in the open along with other 'interesting' developments from the Messerschmitt studio. It was still there, deteriorating rapidly, when it was spotted by Robert Woods, Chief Designer at Bell Aircraft, who contrived to have it sent it to the United States, where it was eventually restored and completed, with the help of Voigt himself, as a non-flying mock-up. It formed the basis for the first ever variable-geometry-winged aircraft, the Bell X-5, the sweep angle of which could be changed in flight to one of three pre-sets: 20, 40 and 60 degrees. This aircraft made its first flight on 20 June 1951, the geometry of the wing being varied in flight for the first time on 15 July.

The other two submissions Messerschmitt made were less well developed but somewhat more radical. The P. 1110 did away with the nose air intake, locating the engine much further back in the airframe, with the duct openings on the fuselage shoulders, just forward of the trailing edges of the constant-chord swept wings. The P. 1111 was more adventurous: an all-wing design of near-delta planform with a heavily swept tail fin and rudder, the air intakes of which were located in the forward part of the wing roots. A proposal submitted too late for the competition was a variant of this design, with a wing of narrower chord and a butterfly tail. Under ideal circumstances, all three designs would probably have been built in prototype form and flown against each other, but as it was, none ever progressed beyond a partially completed wooden mock-up.

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Military Channel - Top Ten Submarines

Posted on December 16 2009 at 01:38 AM

From humble beginnings, submarines quickly evolved into the most sophisticated and powerful weapons of war ever devised. Whether patiently stalking their prey in two World Wars or carrying devastating nuclear missiles as a deterrent in the Cold War, these hunters of the deep have played an often unseen but crucial role in the conflicts of the 20th century. From the unexpectedly small to the terrifyingly huge, this program features some of the most innovative and ambitious weapon systems of the past 100 years. Based on scientific analyses, expert opinion, audience polls and technical comparison, we construct a five-point matrix to rank the TOP TEN SUBMARINES of all time.

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Stuka VII

Posted on December 16 2009 at 01:35 AM

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Stuka VI

Posted on December 16 2009 at 01:34 AM

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Stuka V

Posted on December 16 2009 at 01:33 AM

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Stuka IV

Posted on December 16 2009 at 01:32 AM

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Stuka III

Posted on December 16 2009 at 01:31 AM

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Stuka II

Posted on December 16 2009 at 01:29 AM

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Stuka I

Posted on December 16 2009 at 01:28 AM

Few aircraft projected such an evil intent as the unattractive, angular Stuka. It nevertheless personified Nazi blitzkrieg warfare and was an effective dive-bomber when unopposed, but it wilted quickly in the face of fighter opposition.

In 1933 German aerial expert Ernst Udet witnessed dive-bombing in the United States, which convinced him of similar applications for Europe. The embryonic Luftwaffe had been envisioned as aerial artillery for Wehrmacht land forces, and Udet urged creation of a new Sturzkampfflugzeug (Stuka) forces. A Junkers design team under Hans Pohlmann fielded a prototype in 1935, which was unlike any airplane ever built. Angular and ugly, the Ju 87 was an all-metal monoplane with unmistakable “cranked” wings and trousered landing gear. A crew of two sat back-to-back in a short greenhouse canopy. Test flights proved the new craft to be somewhat slow and sluggish yet highly accurate while diving. Several saw combat during the Spanish Civil War, where they operated with great effect against weak enemy opposition. When World War II commenced, only 500 Ju 87s were in the Luftwaffe inventory, but they wielded a tactical and psychological impact far greater than mere numbers suggested.

The screaming, precision-bombing Stukas epitomized blitzkrieg warfare as they blasted a path for oncoming German tanks and infantry. Their effect upon unarmed civilians was terrifying, for Stukas emitted a loud, high-pitched howl as they nosed over, giving the impression of giant birds of prey. The Ju 87s functioned brilliantly until the Battle of Britain in 1940, where effective fighter opposition caused heavy losses. Thereafter, Stukas were assigned to secondary theaters like the Aegean and Mediterranean with good results. They also enjoyed startling success against Russia, where on September 23, 1941, Hans-Ulrich Rudel destroyed the battleship Marat with a single 2,200- pound bomb, and ultimately accounted for 511 tanks. Stukas rendered good work wherever the Luftwaffe enjoyed air superiority, but by late 1944 they had faded from the scene entirely. More than 5,000 had been constructed.

Type: Dive-Bomber

Dimensions: wingspan, 49 feet, 2 inches; length, 37 feet, 8 inches; height, 12 feet, 9 inches

Weights: empty, 8,686 pounds; gross, 14,550 pounds

Power plant: 1 × 1,500–horsepower Junkers Jumo 211P liquid-cooled in-line engine

Performance: maximum speed, 248 miles per hour; ceiling, 27,885 feet; range, 410 miles

Armament: 2 × 7.92mm machine guns; 2 × 20mm cannons; up to 6,000 pounds of bombs

Service dates: 1936–1945

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Mig-5 Long-range Escort Fighter

Posted on December 15 2009 at 12:20 AM

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Fact File Japanese B1 Type Submarine

Posted on December 13 2009 at 06:12 AM

The largest class of Imperial Navy submarine was the 20-boat B1 Type. 1-35 is the subject of this profile. The B1 Type epitomized the Imperial Navy's large scout submarines with a long-range, aircraft-handling capability, and heavy armament. The B1 Type kept the catapult forward as on earlier aircraft handling submarines, but the hangar was faired into the conning tower, improving underwater performance. 1-35 was completed in August 1942 and had a fairly typical career. She conducted several supply missions to Kiska Island in the Aleutians before being rammed and sunk by destroyer USS Frazier (00-607) on November 23, 1943 off Tarawa in the Gilbert Islands.

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JAPANESE SUBMARINE COLOR SCHEMES

Posted on December 13 2009 at 06:11 AM

All Imperial Navy submarines were originally painted in a dark gray, typically with several markings. The hull number was carried on both sides of the conning tower, either painted on or placed on a canvas marker that could be removed to obscure the boat's identity. This was often accompanied by a representation of the Japanese national ensign. On May 6, 1942, 1-8 was mistakenly bombed by a Japanese aircraft off Kwajalein Island. After this, double white bands were painted on the decks of Japanese submarines as a recognition symbol.

The Imperial Navy did not utilize a well-developed system of warship camouflage during the Pacific War, but some submarines did carry camouflage measures. The Japanese believed that darker colors were harder to spot underwater and in lower visibility; accordingly, many boats were painted in an overall black scheme at the start of the war. A variation was to paint the boat's upper surfaces black, leaving the horizontal surfaces gray. Some boats employed a disruptive camouflage pattern using unknown dark colors over the original gray. Any such camouflage was instituted by the local commander.

During the war, the effectiveness of the Imperial Navy's submarine camouflage schemes was questioned, and the use of black reviewed. The "Submarine Hull Camouflage Experiment" was carried out by units attached to the Submarine School at Kure between December 1944 and March 1945. Ten older submarines participated in the study together with reconnaissance aircraft. Using paint transferred from the Germans, the Imperial Navy tested the effectiveness of the German light gray with four other colors - the standard Japanese black and gray, and two experimental colors, No.2 and No.5.

The results indicated that black was the most ineffective while the boat was surfaced, but the most effective when submerged. The German light gray was found to be ineffective in the waters off Japan. Color NO.2 (light gray with a blue-gray additive) proved the best on a surfaced submarine. However, after all this effort, it is unclear if the results of this test were applied to the Imperial Navy's surviving submarines for the last months of the war.

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SOMUA Cavalry Tank

Posted on December 13 2009 at 06:10 AM

The French SOMUA cavalry tank, known variously as the S-35 or the 35.S, was one of the most effective tanks of the 1940 conflict.

The French Army configured its tank force by branch, with the cavalry force procuring its own armoured vehicles. Cavalry doctrine in 1935 called for the new light mechanised divisions (DLM: Division Legere Mecanique) to serve as the mobile, long-range tools of the high command, capable of launching 'brutal, surprise attacks'. A new tank was needed to carry out this mission, and Schneider's SOMUA plant at St. Ouen near Paris was assigned the task. SOMUA is the acronym for the plant's full name: Societe d'Outillage Mecanique et d'Usinage d'Artillerie. It was one of the first tanks to make extensive use of cast armour. Its APX1-CE turret was similar to that adopted on the Char B1, but used a wider turret ring which led to some changes in the shape of the casting.

After completing a prototype in April 1935, production began late in 1937. The first batch of 50 were delivered to squadrons of the 4th Cuirassiers and 18th Dragoons in Reims for operational trials. By May 1940, a total of 600 were on order of which 395 had been completed.

They were used primarily to arm the DLM which had a nominal strength of 96 SOMUA cavalry tanks in two regiments. In reality, only three DLM had received the SOMUA by the outbreak of the war (1er, 2e, and 3e DLM) as well as one regiment in the 4e DCR (Division Cuirassee de Reserve). Some other units received tanks in the frantic months of May-June 1940 as well, and by the time of the armistice, a total of 429 had been delivered.

The SOMUA S-35 saw extensive combat in Belgium and the later fighting in France. The SOMUA was arguably the best tank in French service in 1940, but its combat performance was mixed. On the one hand, it had excellent armour and firepower. On the other hand, its suspension was antiquated, too few tanks were fitted with radios to permit co-ordinated tactics, and the one-man turret was a drawback in tank-versus-tank fighting.

The Germans acquired 297 SOMUA tanks after the armistice, after allowing the plant to complete some undelivered tanks! Called PzKpfw 35 S 739 (f) in Wehrmacht service, one of the few standard modifications was to cut off the top of the turret cupola and add hatches to permit the commander to operate with his head outside the turret.

The first use of the German SOMUA tanks came in 1941 when 15 were assigned to armoured train units with E.Pz.Zuge 26 through 28 receiving three each and Zuge 29 through 31 receiving two each. These were operated from flatcars, and could disembark from the railroad to chase partisans if necessary. About 60 were converted into artillery tractors, and their surplus turrets deployed on the Atlantic Wall. The remaining SOMUA were assigned to various tank units, mostly for secondary missions. This included a tank company of the SS-Totenkopf Division, which used them for anti-partisan operations; 6/Pz.Rgt. 100 which used them in combat in Normandy in 1944; Pz.Rgt. 201 which used them for training in France in 1941 -42; 1/Pz.Rgt. 202 which used them for partisan fighting in the Balkans from 1942 on; Pz.Rgt. 204 which used them in fighting in the Crimea in 1942; 1/Pz.Abt. 211 which deployed them in Finland; and 2/Pz.Abt. 214 which deployed them in Norway.

Germany sold or gave 40 SOMUA to its allies. Italy received 32, which were mostly deployed with the 200th Tank Battalion at Delianova on Sardinia. Hungary received two for trials purposes in 1943. Bulgaria attempted to order some PzKpfw I light tanks for training purposes, but were provided with six SOMUA instead in February 1944. They were not used by the army, but assigned to border guard and police units for anti-partisan fighting along the frontier in 1944.

The SOMUA also saw later combat service in the French army. After the 1940 armistice, 23 were delivered to North Africa and following Operation Torch in November 1942, they joined with Free French Forces with the 12e Regiment de Chasseurs d'Afrique. This tank unit fought in the Tunisia campaign starting in December 1942, and then was deployed to Senegal in January 1943. At least five SOMUA were hidden during the German occupation in the Massif Central and during the 1944 Normandy fighting, SOMUA were captured by the Allies in German depots. Some of these were reduce German pockets along the; the German SOMUA used in anti-partisan operations in Yugoslavia were captured by partisan units and put into use, and at least one was used by the Yugoslav 1st Tank Brigade alongside its M3A3 Stuarts.

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Mitsubishi J2M Raiden

Posted on December 11 2009 at 07:08 AM

Although a product of the same design team, headed by Jiro Horikoshi, that had given the Imperial Japanese Navy its important A6M Zero, the Mitsubishi J2M was not to enjoy the same degree of success. The very different purpose for which its specification was written probably had some bearing on this, for theJ2Mwas the first single-seat fighter to be procured by the navy for the specific role of interception. The specification was drawn up at a time when Japan was anxious to establish the so-called Greater East Asia Co-Prosperity Sphere and there may well have been a realisation that captured territory would need quick-response active defence. Consequently, the new fighter was required to climb to 19,685 ft (6000 m) for an interception in about 5 minutes and to have a speed of some 373 mph (600 km/h) at that altitude. The resulting J2M1 prototypes were of cantilever low-wing monoplane configuration with a conventional tail unit and retractable tailwheel landing gear. Construction was all-metal, with fabric-covered control surfaces, but the high performance requirement meant that a powerful engine was essential. Because of demands on engine production choice was limited, and selection of the large-diameter 1,430-hp (1066-kW) Mitsubishi Kasei (Mars) 13 radial engine meant that extra effort was needed to keep fuselage drag as low as possible. This factor explains the unusual installation of the engine, with an extension shaft between it and the reduction gear so that the nose entry could be of minimum diameter.

The first of the prototypes was flown on 20 March 1942, but although testing showed that the aircraft handled easily there were problems with the landing gear mechanism and pilots complained that the low-drag curved windscreen distorted the view. As testing continued it was found that the J2M could not meet the climb and high speed requirements. To gain the required performance improvement the fourth airframe was modified to accept the more powerful MK4R-A Kasei 23a engine and, at the same time, the windscreen was modified to incorporate optically flat panels. In this form the aircraft was designated J2M2 and it was this version that was accepted for production by the navy in October 1942 under the official designation Navy Interceptor Fighter Raiden Model 11. But despite the improvements the development and production of this fighter continued to be dogged by problems; it was not until December 1943 that the type began to enter service. By then the J2M3 version was beginning to come off the production line, and this was the most extensively built, about 430 being completed. It differed from the J2M2 by detail improvements to rectify some of the shortcomings, but particularly in revision of the armament, with the fuselage-mounted machine-guns removed and the cannon supplemented by two extra and faster-firing wing-mounted 20-mm cannon; a later variant, designated J2M3a, had all four of the wing-mounted cannon of the Mk 2 faster-firing type. The urgent need to improve high-altitude performance led first to the construction of two J2M4 Model 34 prototypes which introduced the turbocharged 1,820-hp (1357-kW) Mitsubishi MK4R-C Kasei 23c engine, and testing showed that this version was capable of a speed of 362 mph (583 km/h) at 30,185 ft (9200 m), but unreliability of the turbochargers led to development of this version being abandoned. Instead, work was concentrated on the J2M5 which had basically the same airframe as the J2M4, but which was powered by a 1,820-hp (1357-kW) MK4U-4 Kasei 26a radial which incorporated a mechanically-driven three-stage supercharger. This was shown to be reliable, and the J2M5 demonstrated a maximum speed of 382 mph (615 km/h) at 22,310 ft (6800 m) during official tests. Ordered into production with a redesigned cockpit canopy and the same armament as the J2M3, the J2M5, and J2M5a which had the same armament as the J2M3a, were the last production versions of the Raiden. A single experimental J2M6 was flown, this being a conversion of a J2M3 airframe with a wider cockpit, J2M3 armament and the redesigned canopy of the J2M5, but the projected J2M6a, J2M7 and J2M7a which would have introduced armament and engine changes were not built.

Allocated the Allied codename 'Jack', the J2M first saw operational use during 1944 and continued in service until the end of the Pacific War, playing a more conspicuous and vital role as the defensive perimeter became little more than Japan's home islands. In the closing stages J2Ms gained notable success against Allied bombers, and it was either unfortunate for the Japanese or lucky for the Allies that the J2M was not more reliable and available in greater numbers.

Production

A total of 621 aircraft were built by Mitsubishi Jukogyo K.K in Nagoya and Suzuka plants. 128 J2M3 were built by Koza Kaigun Kokusho (Koza Naval Air Arsenal).

• J2M1 - 8 aircraft.

• J2M2 - 131 aircraft. (approximately)

• J2M3 - 307 aircraft built by Mitsubishi and 128 aircraft built by Koza KK.

• J2M4 - 2 aircraft. (including one J2M3 converted to J2M4 standard)

• J2M5 - 43 aircraft.

• J2M6 - 2 aircraft

Specification

Mitsubishi J2M3 Raiden

Type: single-seat interceptor fighter

Powerplant: one 1,820-hp (1357-kW) Mitsubishi MK4R-A Kasei 23a 14-cylinder radial piston engine

Performance: maximum speed 371 mph (597 km/h) at 19,360 ft (5900 m); cruising speed 219 mph (352

Km/h) at 9,840 ft (3000 m); service ceiling 38,385 ft (11700 m); maximum range 655 miles (1055 km)

Weights: empty 5,423lb (2460 kg); maximum take-off 8,695 lb (3945 kg)

Dimensions: span 35 ft 5 ¼ in (10.80 m); length 32 ft 7 ¾ in (9.95 m); height 12 ft 11 ½ in (3.95 m); wing area 215.82 sq ft (20.05 m2)

Variants

J2M1

Prototype fitted with the 1,044 kW (1,400 hp) Mitsubishi MK4C Kasei 13 14-cylinder air-cooled radial engine, and armed with two 7.7 mm (.303 in) Type 97 machine guns in the upper fuselage and two wing-mounted 20 mm Type 99 Model II cannon.

J2M2 Model 11

Fitted with the 1,357 kW (1,820 hp) Mitsubishi MK4R-A Kasei 23a 14-cylinder radial engine, same armament as the J2M1.

J2M3 Model 21

Mitsubishi MK4R-A Kasei 23a engine, two wing-mounted 20 mm Type 99 Model II cannon and two wing-mounted 20 mm Type 99 Model I cannon.

J2M3a Model 21A

Mitsubishi MK4R-A Kasei 23a engine, four wing-mounted 20 mm Type 99 Model II cannon.

J2M4 Model 32

Prototype fitted with the 1,357 kW (1,820 hp) Mitsubishi MK4R-C Kasei 23c engine. Many armament configurations have been reported, e.g., fuselage-mounted oblique-firing 20 mm Type 99 Model I cannon designed to fire upward as it passed underneath a bomber, two wing-mounted 20 mm Type 99 Model II cannon, and two wing-mounted 20 mm Type 99 Model I cannon (some J2M3s were also modified in the field to this configuration). However, no solid evidence exists that the prototypes ever flew armed.

J2M5 Model 33

Increased size, weight and speed at the expense of shorter range (just over half that of the J2M2 and J2M3), turbocharged 1,357 kW (1,820 hp) Mitsubishi MK4U-A Kasei 26a engine, two 20 mm Type 99 cannon in fuselage, two 20 mm Type 99 Model II cannon in wings.

J2M5a Model 33A

Four wing-mounted 20 mm Type 99 Model II cannon. Now, all four wing cannon were harmonized in trajectory and ballistics performance like the Kawanishi N1K-J Shiden fighters, but with more ammunition than they had (200 v. 70-125 rpg). The 20x101 mm cartridge gave the 128 g HE (6-8%) projectile an effective range of 1,000 m (3,280 ft) and a muzzle velocity of 750 m/s. The rate of fire was only 500 rpm each however (down from 520 rpm for the Type 99 Model I which only had a muzzle velocity of 600 m/s and a range of 730 m/2,400 ft with its 20x72 mm cartridge).

J2M6 Model 31

Chronologically earlier than J2M4 and J2M5 this version was based on J2M3. Had wider cockpit and improved bubble canopy later used in J2M3 built since July 1943.

J2M6a Model 31A

Chronologically earlier than J2M4 and J2M5 this version was based on J2M3a. Had wider cockpit and improved bubble canopy later used in J2M3a built since July 1943. One J2M6a was built.

J2M7 Model 23A

J2M3 powered by Kasei 26a engine, none built.

J2M7a Model 23A

J2M3a powered by Kasei 26a engine, none built.

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Early German Armoured Cars

Posted on December 11 2009 at 07:08 AM

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WEAPONS OF THE MEXICAN WAR 1846–1847

Posted on December 08 2009 at 06:25 AM

United States Weapons

The weapons of the U.S. soldiers in the Mexican-American War included muskets and rifles, pistols, Colt revolvers, bayonets and swords, and artillery pieces. The high quality and reliability of the U.S. weapons, and the mobility of the Flying Artillery, gave the U.S. soldiers a distinct advantage over their Mexican counterparts.

The .69-caliber, smoothbore flintlock musket was standard issue for the U.S. soldier. It had an effective range of about 100 yards. About ten different models were used during the war, the most famous being the 1822 model. Some troops also carried the Hall breech-loading flintlock rifle or the Model 1841 percussion musket (also called the “Mississippi rifle”). Relatively few men carried percussion rifles. Many officers carried double-barreled shotguns for close combat. Dragoons also occasionally were armed with breech-loading Hall carbines with a shorter barrel.

Standard sidearms were flintlock or percussion smoothbore pistols that were inaccurate beyond a range of 10 or 15 yards. Other troops, most notably officers and Texas Rangers, carried the more expensive Colt revolver. The Hartford Courant reported that “each arm is calculated to hold six charges, which may be fired in as many seconds, and again reloaded as quickly as an ordinary fire arm. The regiment of the United States Mounted Rifles, for whom a thousand of these arms have been made...can fire a volley of six thousand balls into an enemy’s ranks, without loading, and afterwards load and fire at the rate of six thousand charges per minute.” The Colt, of course, was effective only in close quarters, such as colliding cavalry charges or hand-to-hand combat. Other weapons included swords, bayonets, and Bowie knives.

The biggest U.S. weapons advantage was its artillery. U.S. guns fired cannonballs, shells (explosive charge with fuse), spherical case (container with lead balls and explosives), and canister (tin can filled with 27 lead balls packed in sawdust). Canister was effective up to about 300 yards. The artillery consisted of long-barreled cannon, howitzers (short-barreled, lightweight guns), and mortars of various weights, cast from iron or bronze. The highly trained and disciplined Flying Artillery units could fire every 10 or 15 seconds, more than five times faster than Mexican artillery. Used mostly to inflict casualties, the Flying Artillery moved rapidly to where it was most needed on the battlefield, and usually created gaping holes in the enemy lines.

Mexico Weapons

The weapons of the Mexican soldiers were typically smoothbore flintlock muskets, pistols, sabers and shorter swords, lances, and antiquated cannon. Mexican weaponry was older and less reliable than U.S. weapons, especially the older, heavier cannon and its ammunition.

Mexico, which did not own an operating armory, purchased its weapons from European dealers. Most infantrymen were outfitted with older .753-caliber, smoothbore flintlock muskets from the 1830s. The British Tower-type smoothbore musket, which the British government no longer favored, was purchased in large quantities at discount prices. Called the “Brown Bess,” its range was less than 100 yards. A lesser number of 1838-style British Baker rifles were also used, but, because they were expensive and of better quality, they were saved for the elite troops and sharpshooters. After the Battle of Cerro Gordo, George Ballentine commented that “we found the road strewed with the muskets and bayonets which the Mexicans had thrown away in their hasty retreat. All of these muskets were of British manufacture and had the Tower mark on their locks. They were old and worn out, having evidently been condemned as unserviceable in the British army and then sold to the Mexicans at a low price.... After examining a few of them I came to the conclusion that for efficient service one of our muskets was equal to at least three of them.”

The variable quality and style of muskets created a host of problems for the Mexican soldiers, especially in matching ammunition. During the Battle of Churubusco in August 1847, the Mexican soldiers were infuriated by the fact that their lead balls were too large and frequently jammed in the musket barrel. Because of inferior powder, they were also forced to overcharge their rifles, and the resulting kick made them fire high. The British Paget flintlock carbine, and the escopeta, an old-fashioned, Napoleonic variety of blunderbuss, were also used by cavalrymen.

Cavalrymen were equipped with lances, sabers, and carbines. In the hands of an experienced horseman the lance was a formidable weapon. In addition to the four cutting edges of the eight-inch blade, a flag at the tip was meant to frighten the enemy’s horse. Lancers were some of the most highly regarded units in the Mexican army, and their attacks had great shock value.

Mexican artillerymen fired the antiquated Griveaubal cannon of different calibers, for which there was limited ammunition. Mexican cannoneers, especially in the beginning of the war, favored the use of solid shot in trying to knock out opposing batteries (in comparison, the U.S. artillery strategy was to destroy groups of soldiers). Toward the end of the war, during U.S. General Winfield Scott’s march to Mexico City and Colonel Alexander Doniphan’s march to Chihuahua, some cannons were cast in local foundries. Although the artillerists were well trained, the cannon were often defective. Uneven or inferior gunpowder overshot projectiles or made them fall dangerously short. The artillery was drawn by civilian carts and drivers, or often hauled by mules—the Mexican army did not have professional teamsters.

Notes:

1. Gregory J. W. Urwin, The United States Infantry, An Illustrated History: 1775-1918, Sterling Publishing Company, Inc., New York, New York, 1991, Page 66. Although the U.S. Army had officially adopted the percussion system by the time of the Mexican War, resistance from General Winfield Scott meant that most of his regular infantrymen began the march to Mexico City with flintlock muskets. In the general’s preparations for the invasion of Vera Cruz, Scott requested that his soldiers be armed with flintlocks in order to standardize logistics. He was concerned about the supply of percussion caps over perilous routes. Flints, unlike percussion caps, could always be located, manufactured, or captured. However, by the end of the war, the U.S. Army had issued more than twice as many percussion caps as flints, a clear sign of the military’s transition to percussion weapons. (For example, Company A, 4th U.S. Artillery reported on June 30, 1847 that it was equipped with 87 percussion muskets and only 14 old-style flintlocks.)

2. Firearm experts continue to disagree on whether or not the Model 1816 Type II musket, manufactured between 1822 and 1831, should be officially referred to as the Model 1822. Although the Model 1816 flintlock musket was one of the most common weapons of the Mexican War, no other regulation firearm has been the subject of as much controversy concerning its proper designation. Early authorities have, in addition to the Model 1816 designation, referred to this particular musket as either Model 1821, 1822 or 1831.” The U.S. Musket, Model 1816, is one of the arms that has badly confused the student, because the proper interpretation has not been placed on Wadsworth’s letters. The failure to use the correspondence which portrays the build-up, adoption, and improvements made to this model, together with later ordnance records referring to it as the model of 1822, has all tended to confuse the experts. Duplication of these weapons proved unsatisfactory and the Springfield Armory further confused production by adding improvements after the prototypes were released. Negotiations with contractors continued until 1822, when the final design was decided. Thirty prototype muskets marked “MODEL 1822" were provided to various contractors. The hundreds of thousands of weapons produced became typed as the Model 1822 thereafter. Firearm authority Arcadi Gluckman in his 1959 milestone book entitled, “Identifying Old U.S. Muskets, Rifles And Carbines” refers to this flintlock weapon as the Model 1816, citing an 1816 document which authorized the original prototypes made in 1817. Gluckman ignored the 1841 Ordnance Manual and the nomenclature it set forth for this weapon, “Model 1822.” Unfortunately, the controversy remains unresolved with experts firmly entrenched on both sides of the issue.

3. Joseph G. Bilby, Civil War Firearms, Combined Publishing, Conshohocken, Pennsylvania, 1996, Pages 19 and 32. Single ball loads for the .69 caliber Model 1816 fired undersized .64 caliber projectiles to facilitate quick loading, at the expense of accuracy. The cartridge paper around the ball helped to fill up the “windage” or clearance between the diameter of the undersized ball and the .69 caliber barrel, providing some benefits of a patch. Page 20. In the 1840's the caliber of the American musket ball was increased to .65 and the gun’s powder charge was reduced from 130 to 110 grains. Although accuracy improved somewhat, most military men continued to rely on multiple projectiles to improve combat hit ratios. Pages 18,19 and 20. By the time of the American Revolution it was common practice to load smaller buckshot along with a musket ball in paper cartridges used in .69 and .75 caliber muskets. The number of buckshot per cartridge varied. In October 1777, General George Washington recommended that his men deliver their first volley with a load of “one musket ball and four or eight buckshot, according to the strength of their pieces.” Single-ball, buck and ball, and straight buckshot loads of from twelve to fifteen pellets remained part of the American military ammunition inventory after the Revolutionary War. Due to limited effective range of straight buckshot loads, they were largely used as guard cartridges, while buck and ball became the military’s favored musket load. Between 1835 and 1840, three times as many buck and ball cartridges, loaded with a standard musket ball and three buckshot, were issued by the U.S. Ordnance Department as were single ball loads.

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Ship gun fire-control systems

Posted on December 08 2009 at 06:23 AM

Ship gun fire-control systems (GFCS) enable remote and automatic targeting of guns against ships, aircraft, and shore targets, with or without the aid of radar or optical sighting. Most US ships destroyers or larger (but not destroyer escorts or escort carriers) employed GFCS for 5 inch and larger guns, up to battleships such as the USS Iowa. After the 1950s, GCFSs were integrated with missile fire-control systems and other ship sensors.

The major components of a GFCS are a manned director, with or replaced by radar or television camera, a computer, stabilizing device or gyro, and equipment in a plotting room [1] The brains were first provided by the Mark 1A Fire Control Computer which was an electro-mechanical analog ballistic computer that provided quick and accurate near real-time first-shot hit firing solutions which could automatically control one or more gun mounts against stationary, or moving targets on the surface or in the air. This gave American forces a technological advantage in WWII against the Japanese who did not develop this technology, and still used visual correction of shots with colored splashes. Digital computers would not be adopted for this purpose by the US until the mid 1970s. However, it must be emphasized that all analogue AA fire control systems had severe limitations, and even the USN Mk 37 required nearly 1000 rounds of 5" mechanical fuze ammunition per kill, even in late 1944. [2]

Mk 37 Director c1944 with Mk 12 (rectangular antenna) and Mk 22 "orange peel"

The MK 37 was the first of a series of evolutionary improvements in gun fire control systems.

1. History

Naval fire control is more complex than for single ground-based gun because of the need to control the firing of several guns at once. In naval engagements both the firing guns and target are moving, and the variables are compounded by the greater distances and times involved. Furthermore, a ship rolls and pitches, making gyroscopic stabilization extremely desirable. Naval gun fire control potentially involves three levels of complexity. Local control originated with primitive gun installations aimed by the individual gun crews.

The director system of fire control was pioneered by British navy in 1912. All guns were laid from a central position placed above the bridge as high as possible. The director became a design feature of battleships, with Japanese pagoda-style masts designed to maximize the view of the director over long ranges. A fire control officer who ranged the salvos transmitted elevations and angles to individual guns. Coordinated gunfire from a formation of ships at a single target was a focus of battleship fleet operations. Corrections are made for surface wind velocity, firing ship roll and pitch, powder magazine temperature, drift of rifled projectiles, individual gun bore diameter adjusted for shot-to-shot enlargement, and rate of change of range with additional modifications to the firing solution based upon the observation of preceding shots.

Rudimentary naval fire control systems were first developed around the time of World War I. For a description of one, see US Naval Fire Control, 1918.

For the UK, their first system was built before the Great War. At the heart was an analogue computer designed by Commander (later Admiral Sir) Frederic Charles Dreyer that calculated rate of change of range. The Dreyer Table was to be improved and served into the interwar period at which point it was superseded in new and reconstructed ships by the Admiralty Fire Control Table. [3]

The use of Director controlled firing together with the fire control computer moved the control of the gun laying from the individual turrets to a central position, although individual gun mounts and multi-gun turrets may retain a local control option for use when battle damage limits Director information transfer. Guns could then be fired in planned salvos, with each gun giving a slightly different trajectory. Dispersion of shot caused by differences in individual guns, individual projectiles, powder ignition sequences, and transient distortion of ship structure was undesirably large at typical naval engagement ranges. Directors high on the superstructure had a better view of the enemy than a turret mounted sight, and the crew operating it were distant from the sound and shock of the guns.

Unmeasured and uncontrollable ballistic factors like high altitude temperature, humidity, barometric pressure, wind direction and velocity required final adjustment through observation of fall of shot. Visual range measurement (of both target and shell splashes) was difficult prior to availability of RADAR. The British favoured coincident rangefinders while the Germans and the U.S. Navy, stereoscopic type. The former were less able to range on an indistinct target but easier on the operator over a long period of use, the latter the reverse.

In a typical WWII British ship the fire control system connected the individual gun turrets to the director tower (where the sighting instruments were) and the analogue computer in the heart of the ship. In the director tower, operators trained their telescopes on the target; one telescope measured elevation and the other bearing. Rangefinder telescopes on a separate mounting measured the distance to the target. These measurements were converted by the Fire Control Table into bearings and elevations for the guns to fire on. In the turrets, the gunlayers adjusted the elevation of their guns to match an indicator which was the elevation transmitted from the Fire Control table - a turret layer did the same for bearing. When the guns were on target they were centrally fired. [4]

In the Battle of Jutland, while the British were thought by some to have the finest fire control system in the world at that time, during the Battle of Jutland only 3% of their shots actually struck their targets. At that time, the British primarily used a manual fire control system. The one British ship in the battle that had a mechanical fire control system turned in the best shooting results. [5] This experience contributed to computing rangekeepers becoming standard issue. [6]

The US Navy's first deployment of a rangekeeper was on the USS Texas (BB-35) in 1916. Because of the limitations of the technology at that time, the initial rangekeepers were crude. For example, during World War I the rangekeepers would generate the necessary angles automatically but sailors had to manually follow the directions of the rangekeepers. This task was called "pointer following" but the crews tended to make inadvertent errors when they became fatigued during extended battles. [7] During World War II, servomechanisms (called "power drives" in the U.S. Navy) were developed that allowed the guns to automatically steer to the rangekeeper's commands with no manual intervention, though pointers still worked even if automatic control was lost. The Mk. 1 and Mk. 1A computers contained approx. 20 servomechanisms, mostly position servos, to minimize torque load on the computing mechanisms. [8]

During their long service life, rangekeepers were updated often as technology advanced and by World War II they were a critical part of an integrated fire control system. The incorporation of radar into the fire control system early in World War II provided ships the ability to conduct effective gunfire operations at long range in poor weather and at night. [9]

The Aichi Clock Company first produced the Type 92 Shagekiban Low Angle analog computer in 1932. The USN Rangekeeper and the Mark 38 GFCS had an edge over Imperial Japanese Navy systems in operability and flexibility. The US system allowing the plotting room team to quickly identify target motion changes and apply appropriate corrections. The newer Japanese systems such as the Type 98 Hoiban and Shagekiban on the YAMATO class were more up to date, which eliminated the Sokutekiban, but it still relied on 7 operators. In contrast to US radar aided system, the Japanese relied on averaging optical range finders, lacked gyros to sense the horizon, and required manual handling of follow-ups on the Sokutekiban, Shagekiban, Hoiban as well as guns themselves.

This could have played a role in Center Force’s battleships dismal performance in the Battle off Samar in October 1944. [10] In that action, destroyers pitted against the world's largest armored battleships and cruisers dodged shells to within torpedo firing range, while lobbing hundreds of accurate automatically-aimed 5 inch rounds on target. Cruisers did not land hits on splash-chasing escort carriers until after an hour of pursuit to close within 5 miles. Although the Japanese pursued a doctrine of achieving superiority at long gun ranges, one cruiser fell victim to secondary explosions caused by hits from within the range of carrier-based single "peashooter" 5 in guns. Eventually with the aid of hundreds of carrier based aircraft, a battered center force was turned back just before it could have finished off survivors of the lightly armed task force of screening escorts and escort carriers of Taffy 3. The Battle of the Surigao Strait also established the clear superiority of US radar-assisted systems at night.

The rangekeeper's target position prediction characteristics could be used to defeat the rangekeeper. For example, many captains under long range gun attack would make violent maneuvers to "chase salvos." A ship that is chasing salvos is maneuvering to the position of the last salvo splashes. Because the rangekeepers are constantly predicting new positions for the target, it is unlikely that subsequent salvos will strike the position of the previous salvo. [11] Practical rangekeepers had to assume that targets were moving in a straight-line path at a constant speed, to keep complexity to acceptable limits. A sonar rangekeeper was built to include a target circling at a constant radius of turn, but that function had been disabled.

Only the US achieved 'blindfire' radar fire-control, with no need to visually acquire the opposing vessel. The Axis powers all lacked this capability. Classes such as Iowa and South Dakota could lob shells over visual horizon, in darkness, through smoke or weather. American systems had the best stable vertical elements, so they could keep a solution on a target even during maneuvers. U.S. battleships could both shoot and maneuver, whereas their opponents could only do one or the other. [12] (In today's terminology, stable elements or stable verticals would be called vertical gyros.)

The last combat action for the analog rangekeepers, at least for the US Navy, was in the 1991 Persian Gulf War [13] when the rangekeepers on the Iowa-class battleships directed their last rounds in combat.

2. US Navy Systems

2. 1. MK 33 Gun Fire Control System (GFCS)

The Mk 33 GFCS was a power-driven fire control director, less advanced than the MK 37. It could compute firing solutions for targets moving at up to 320 knots, or 400 knots in a dive. Its installations started in 1941 on aircraft carriers with two Mk 33 directors mounted fore and aft of the island. They had no fire-control radar initially, and were aimed only by sight. After 1942, the directors were equipped with the Mk 4 fire-control radar. With the Mk 4 large aircraft at up to 40,000 yards could be targeted. It had less range against low-flying aircraft, and large surface ships had to be within 30,000 yards. With radar, targets could be seen and hit accurately at night, and through weather. [14] The Mark 33 and 37 systems used tachymetric target motion prediction. [15]

2. 2. MK 37 Gun Fire Control System (GFCS)

Development of the Sperry Mk 1 computer was begun in 1932 as part of the Mk 37 fire control system for the 5"/38 DP mount. The Royal Navy had conducted sea trials of their initial version of the High Angle Control System for AA fire, about two years earlier, in January 1930. The computer was completed as the Ford Mk 1 computer by 1935. Rate information for height changes enabled complete solution for aircraft targets moving over 400 mph. Destroyers starting with the Sims class employed one of these computers, battleships up to four. The system's effectiveness against aircraft diminished as planes became faster, but toward the end of World War II upgrades were made to the Mk37 System, and it was made compatible with the development of the VT (Variable Time) proximity fuze which exploded when it was near a target, rather than by timer or altitude, greatly increasing probability any one shell would destroy a target.

2. 2. 1. Mark 37 Director

Mk 37 Director above bridge of destroyer USS Cassin Young (DD-793) with SPG 25 radar antenna

The function of the Mark 37 Director, which resembles a turret with "ears" rather than guns, was to track the present position of the target in bearing, elevation, and range. To do this, it had optical sights (the rectangular windows or hatches on the front), an optical rangefinder (the tubes or ears sticking out each side), and later models, fire control radar antennas. The rectangular antenna is for the Mark 12 FC radar, and the parabolic antenna on the left ("orange peel") is for the Mk 22 FC radar. They were part of an upgrade to improve tracking of aircraft. [1]

The Director Officer also had a slew sight used to quickly point the director towards a new target. [16] Up to four Mark 37 Gun Fire Control Systems were installed on on battleships. On a battleship, the director is protected by 1.5 inches of armor, and weighs 21 tons. The Mark 37 director aboard the USS Joseph P. Kennedy, Jr. is protected with one-half inch of armor plate and weighs 16 tons. [17]

5 in gun on the Fletcher-class destroyer USS David W. Taylor (DD-551)

Stabilizing signals from the Stable Element kept the optical sight telescopes, rangefinder, and radar antenna free from the effects of deck tilt. The signal that kept the rangefinder's axis horizontal was called "crosslevel"; elevation stabilization was called simply "level". Although the stable element was below decks in Plot, next to the Mk.1/1A computer, its internal gimbals followed director motion in bearing and elevation so that it provided level and crosslevel data directly. To do so, accurately, when the fire control system was initially installed, a surveyor, working in several stages, transferred the position of the gun director into Plot so the stable element's own internal mechanism was properly aligned to the director.

Although the rangefinder had significant mass and inertia, the crosslevel servo normally was only lightly loaded, because the rangefinder's own inertia kept it essentially horizontal; the servo's task was usually simply to ensure that the rangefinder and sight telescopes remained horizontal.

Mk. 37 director train (bearing) and elevation drives were by D.C. motors fed from Amplidyne rotary power-amplifying generators. Although the train Amplidyne was rated at several kW maximum output, its input signal came from a pair of 6L6 audio beam tetrode vacuum tubes (valves, in the U.K.).

2. 2. 2. Plotting Room

In battleships, the Secondary Battery Plotting Rooms were down below the waterline and inside the armor belt. They contained four complete sets of the fire control equipment needed to aim and shoot at four targets. Each set included a Mark 1A computer, a Mark 6 Stable Element, FC Radar controls and displays, Parallax correctors, a switchboard, and people to operate it all.

(In the early 20th century, successive range and/or bearing readings were probably plotted either by hand or by the fire control devices (or both). Humans were very good data filters, able to plot a useful trend line given somewhat-inconsistent readings. As well, the Mark 8 Rangekeeper included a plotter. The distinctive name for the fire-control equipment room took root, and persisted even when there were no plotters.)

2. 2. 3. Ford Mark 1A Fire Control Computer

Mark 1A Computer

The Mark 1A Fire Control Computer was an electro-mechanical analog ballistic computer. Originally designated the Mark 1, design modifications were extensive enough to change it to "Mk. 1A". Sailors would stand around a box 62 inches long, 38 inches wide, and 45 inches high. Even though built with extensive use of an aluminum alloy framework (including thick internal mechanism support plates) and computing mechanisms mostly made of aluminum alloy, it weighed as much as a car, about 3125 lb, with the Star Shell Computer Mark 1 adding another 215 lb. It used 115 volts AC, 60 Hz, single phase, and typically a few amperes or even less. Under worst-case fault conditions, its synchros apparently could draw as much as 140 amperes, or 15,000 watts (about the same as 3 houses while using ovens). Unfortunately, that figure has remained in current references without explanatory qualification. (For a computer that size to dissipate 15 kW with no cooling provisions is absurd.) Almost all of the computer's inputs and outputs were by synchro torque transmitters and receivers.

Its function was to automatically aim the guns so that a fired projectile would collide with the target. [1] This is the same function as the main battery’s Mk 8 Rangekeeper above except that some of the targets the Mark 1A had to deal with also moved in elevation — and much faster. For a surface target, the Secondary Battery’s Fire Control problem is the same as the Main Battery’s with the same type inputs and outputs. The major difference between the two computers is their ballistics calculations. The amount of gun elevation needed to project a 5-in shell nine nautical miles (17 km) is very different from the elevation needed to project a 16-in shell the same distance.

In operation, this computer received target range, bearing, and elevation from the gun director. As long as the director was on target, clutches in the computer were closed, and movement of the gun director (along with changes in range) made the computer converge its internal values of target motion to values matching those of the target. While converging, the computer fed aided-tracking ("generated") range, bearing, and elevation to the gun director. If the target remained on a straight-line course at a constant speed (and in the case of aircraft, constant rate of change of altitude ("rate of climb"), the predictions became accurate and, with further computation, gave correct values for the gun lead angles and fuze setting.

Concisely, the target's movement was a vector, and if that didn't change, the generated range, bearing, and elevation were accurate for up to 30 seconds. Once the target's motion vector became stable, the computer operators told the gun director officer ("Solution Plot!"), who usually gave the command to commence firing. Unfortunately, this process of inferring the target motion vector required a few seconds, typically, which might take too long.

The process of determining the target's motion vector was done primarily with an accurate constant-speed motor, disk-ball-roller integrators, nonlinear cams, mechanical resolvers, and differentials. Four special coordinate converters, each with a mechanism in part like that of a traditional computer mouse, converted the received corrections into target motion vector values. The Mk. 1 computer attempted to do the coordinate conversion (in part) with a rectangular-to polar converter, but that didn't work as well as desired (sometimes trying to make target speed negative!). Part of the design changes that defined the Mk. 1A were a re-thinking of how to best use these special coordinate converters; the coordinate converter ("vector solver") was eliminated.

The Stable Element, which in contemporary terminology would be called a vertical gyro, stabilized the sights in the director, and provided data to compute stabilizing corrections to the gun orders. Gun lead angles meant that gun-stabilizing commands differed from those needed to keep the director's sights stable. Ideal computation of gun stabilizing angles required an impractical number of terms in the mathematical expression, so the computation was approximate.

To compute lead angles and time fuze setting, the target motion vector's components as well as its range and altitude, wind direction and speed, and own ship's motion combined to predict the target's location when the shell reached it. This computation was done primarily with mechanical resolvers ("component solvers"), multipliers, and differentials, but also with one of four three-dimensional cams.

Based on the predictions, the other three of the three-dimensional cams provided data on ballistics of the gun and ammunition that the computer was designed for; it could not be used for a different size or type of gun except by rebuilding that could take weeks.

Servos in the computer boosted torque accurately to minimize loading on the outputs of computing mechanisms, thereby reducing errors, and also positioned the large synchros that transmitted gun orders (bearing and elevation, sight lead angles, and time fuze setting).These were electromechanical "bang-bang", yet had excellent performance.

The anti-aircraft fire control problem was more complicated because it had the additional requirement of tracking the target in elevation and making target predictions in three dimensions. The outputs of the Mk 1A were the same (gun bearing and elevation), except fuze time was added. The fuze time was needed because the ideal of directly hitting the fast moving aircraft with the projectile was impractical. With fuze time set into the shell, it was hoped that it would explode near enough to the target to destroy it with the shock wave and shrapnel. Towards the end of World War II, the invention of the VT proximity fuze eliminated the need to use the fuze time calculation and its possible error. This greatly increased the odds of destroying an air target. Digital fire control computers were not introduced into service until the mid 1970s.

Central aiming from a gun director hasa minor complication in that the guns are often far enough away from the director to require parallax correction so they aim correctly. In the Mk. 37 GFCS, the Mkk1 / 1A sent parallax data to all gun mounts; each mount had its own scale factor (and "polarity") set inside the train (bearing) power drive (servo) receiver-regulator (controller).

Twice, in its history, internal scale factors were changed, presumably by changing gear ratios. Target speed had a hard upper limit, set by a mechanical stop. It was originally 300 knots, and subsequently doubled in each rebuild.

These computers were built by Ford Instrument Company, Long Island City, Queens, New York. The company was named after Hannibal C. Ford, a genius designer, and principal in the company. Special machine tools machined face cam grooves and accurately duplicated 3-D ballistic cams.

Generally speaking, these computers were very well designed and built, very rugged, and almost trouble-free, Frequent tests included entering values via the handcranks and reading results no the dials, with the time motor stopped. These were static tests. Dynamic tests were done similarly, but used gentle manual acceleration of the "time line" (integrators) to prevent possible slippage errors when the time motor was switched on; the time motor was switched off before the run was complete, and the computer was allowed to coast down. Easy manual cranking of the time line brought the dynamic test to its desired end point, when dials were read.

As was typical of such computers, flipping a lever on the handcrank's support casting enabled automatic reception of data and disengaged the handcrank gear. Flipped the other way, the gear engaged, and power was cut to the receiver's servo motor.

The mechanisms (including servos) in this computer are described superbly, with many excellent illustrations, in the Navy publication OP 1140.

There are photographs of the computer's interior in the National Archives; some are on Web pages, and some of those have been rotated a quarter turn.

2. 2. 4. Stable Element

Mark 6 Stable Element

The function of the Mk 6 Stable Element (pictured) in this fire control system is the same as the function of the Mk 41 Stable Vertical in the main battery system. It is a vertical seeking gyroscope ("vertical gyro", in today's terms) that supplies the system with a stable up direction on a rolling and pitching ship. In surface mode, it replaces the director’s elevation signal. [1] It also has the surface mode firing keys.

It is based on a gyroscope that erects so its spin axis is vertical. The housing for the gyro rotor rotates at a low speed, on the order of 18 rpm. On opposite sides of the housing are two small tanks, partially filled with mercury, and connected by a capillary tube. Mercury flows to the lower tank, but slowly (several seconds) because of the tube's restriction. If the gyro's spin axis is not vertical, the added weight in the lower tank would pull the housing over if it were not for the gyro and the housing's rotation. That rotational speed and rate of mercury flow combine to put the heavier tank in the best position to make the gyro precess toward the vertical.

When the ship changes course rapidly at speed, the acceleration due to the turn can be enough to confuse the gyro and make it deviate from true vertical. In such cases, the ship's gyrocompass sends a disabling signal that closes a solenoid valve to block mercury flow between the tanks. The gyro's drift is low enough not to matter for short periods of time; when the ship resumes more typical cruising, the erecting system corrects for any error.

The Earth's rotation is fast enough to need correcting. A small adjustable weight on a threaded rod, and a latitude scale makes the gyro precess at the Earth's equivalent angular rate at the given latitude. The weight, its scale, and frame are mounted on the shaft of a synchro torque receiver fed with ship's course data from the gyro compass, and compensated by a differential synchro driven by the housing-rotator motor. The little compensator in operation is geographically oriented, so the support rod for the weight points east and west.

At the top of the gyro assembly, above the compensator, right on center, is an exciter coil fed with low-voltage AC. Above that is a shallow black-painted wooden bowl, inverted. Inlaid in its surface, in grooves, are two coils essentially like two figure 8s, but shaped more like a letter D and its mirror image, forming a circle with a diametral crossover. One coil is displaced by 90 degrees. If the bowl (called an "umbrella") is not centered above the exciter coil, either or both coils have an output that represents the offset. This voltage is phase-detected and amplified to drive two DC servo motors to position the umbrella in line with the coil.

The umbrella support gimbals rotate in bearing with the gun director, and the servo motors generate level and crosslevel stabilizing signals. The Mk. 1A's director bearing receiver servo drives the pickoff gimbal frame in the stable element through a shaft between the two devices, and the Stable Element's level and crosslevel servos feed those signals back to the computer via two more shafts.

(The sonar fire-control computer aboard some destroyers of the late 1950s required roll and pitch signals for stabilizing, so a coordinate converter containing synchros, resolvers, and servos calculated the latter from gun director bearing, level, and crosslevel.)

2. 2. 5. Fire Control Radar

The fire-control radar used on the Mk 37 GFCS has evolved. In the 1930’s, the Mk 33 Director did not have a radar antenna. Then in September 1941, the first rectangular Mk 4 Fire-control radar antenna was mounted on Mk 33 and Mk 37 Directors, [18] becoming common in mid 1942. Soon aircraft flew faster, and in c1944 to increase speed and accuracy the Mk 4 was replaced by a combination of the Mk 12 (rectangular antenna) and Mk 22 (parabolic antenna) "orange peel" radars. (pictured) [16] in the late 1950s, Mk. 37 directors had Western Electric Mk. 25 X-band conical-scan radars with round, perforated dishes. Finally, the circular SPG 25 antenna was mounted on top.

2. 3. MK 38 Gun Fire Control System

The Mk38 Gun Fire Control System (GFCS) controlled the large main battery guns of Iowa class battleships. They were a major advance over the primitive radar sets used by the Japanese in World War II. The major components were the director, plotting room, and interconnecting data transmission equipment. The two systems, forward and aft, were complete and independent. Their plotting rooms were isolated to protect against battle damage propagating from one to the other.

2. 3. 1. Director

Mark 38 Director

The forward Mk38 Director (pictured) was situated on top of the fire control tower. The director was equipped with optical sights, optical Mark 48 Rangefinder (the long thin boxes sticking out each side), and a Mark 13 Fire Control Radar antenna (the rectangular shape sitting on top). [1] [19] The purpose of the director was to track the target's present bearing and range. This could be done optically with the men inside using the sights and Rangefinder, or electronically with the radar. (The fire control radar was the preferred method.) The present position of the target was called the Line-Of-Sight (LOS), and it was continuously sent down to the plotting room by synchro motors. When not using the radar's display to determine Spots, the director was the optical spotting station. [1]

2. 3. 2. Plotting Room

USS Missouri's Main Plot, c1950

The Forward Main Battery Plotting Room was located below the waterline and inside the armored belt. [1] It housed the forward system's Mark 8 Rangekeeper, Mark 41 Stable Vertical, Mk13 FC Radar controls and displays, Parallax Correctors, Fire Control Switchboard, battle telephone switchboard, battery status indicators, assistant Gunnery Officers, and Fire Control Technicians (FT's). [1] [19]

Mark 8 Rangekeeper

The Mk8 Rangekeeper was an electromechanical analog computer [1] [19] whose function was to continuously calculate the gun's bearing and elevation, Line-Of-Fire (LOF), to hit a future position of the target. It did this by automatically receiving information from the director (LOS), the FC Radar (range), the ship's gyrocompass (true ship's course), the ships Pitometer log (ship's speed), the Stable Vertical (ship's deck tilt, sensed as level and crosslevel), and the ship's anemometer (relative wind speed and direction). Also, before the surface action started, the FT's made manual inputs for the average initial velocity of the projectiles fired out of the battery's gun barrels, and air density. With all this information, the rangekeeper calculated the relative motion between its ship and the target. [1] It then could calculate an offset angle and change of range between the target's present position (LOS) and future position at the end of the projectile's time of flight. To this bearing and range offset, it added corrections for gravity, wind, Magnus Effect of the spinning projectile, stabilizing signals originating in the Stable Vertical, Earth's curvature, and Coriolis effect. The result was the turret's bearing and elevation orders (LOF). [1] During the surface action, range and deflection Spots and target altitude (not zero during Gun Fire Support) were manually entered.

Mark 41 Stable Vertical

The Mk 41 Stable Vertical was a vertical seeking gyroscope, and its function was to tell the rest of the system which-way-is-up on a rolling and pitching ship. It also held the battery's firing keys. [1]

The Mk 13 FC Radar supplied present target range, and it showed the fall of shot around the target so the Gunnery Officer could correct the system's aim with range and deflection spots put into the rangekeeper. [1] It could also automatically track the target by controlling the director's bearing power drive. [1] Because of radar, Fire Control systems are able to track and fire at targets at a greater range and with increased accuracy during the day, night, or inclement weather. This was demonstrated in November 1942 when the battleship USS Washington engaged the Imperial Japanese Navy battlecruiser Kirishima at a range of 18,500 yards (16,900 m) at night. [20] The engagement left Kirishima in flames, and she was ultimately scuttled by her crew. [21] This gave the United States Navy a major advantage in World War II, as the Japanese did not develop radar or automated fire control to the level of the US Navy and were at a significant disadvantage. [20]

The parallax correctors are needed because the turrets are located hundreds of feet from the director. There is one for each turret, and each has the turret and director distance manually set in. They automatically received relative target bearing (bearing from own ship's bow), and target range. They corrected the bearing order for each turret so that all rounds fired in a salvo converged on the same point.

Fire Control Switchboard

The fire control switchboard configured the battery. [1] With it, the Gunnery Officer could mix and match the three turrets to the two GFCSs. He could have the turrets all controlled by the forward system, all controlled by the aft system, or split the battery to shoot at two targets.

The assistant Gunnery Officers and Fire Control Technicians operated the equipment, talked to the turrets and ship's command by sound-powered telephone, and watched the Rangekeeper's dials and system status indicators for problems. If a problem arose, they could correct the problem, or reconfigure the system to mitigate its effect.

2. 4. MK 51 Fire Control System

Mark 51 Director with Mark 14 (40 mm) Gun Sight

The Bofors 40 mm anti-aircraft guns were arguably the best light anti-aircraft weapon of World War II., [22] employed on almost every major warship in the U.S. and UK fleet during World War II from about 1943 to 1945. [22] They were most effective on ships as large as destroyer escorts or larger when coupled with electric-hydraulic drives for greater speed and the Mark 51 Director (pictured) for improved accuracy, the Bofors 40 mm gun became a fearsome adversary, accounting for roughly half of all Japanese aircraft shot down between 1 October 1944 and 1 February 1945. [22] along with radar directed fire from 5 inch guns.

2. 5. MK 56 Gun Fire Control System (GFCS)

This GFCS was designed toward the end of World War II, apparently in response to Japanese kamikaze aircraft attacks. It was conceived by Ivan Getting, mentioned near the end of his Oral history, and its linkage computer was designed by Antonín Svoboda. Its gun director was not shaped like a box, and it had no optical rangefinder. It was manned by one officer, and had sliprings, permitting continuous rotation. (The Mk. 37 gun director had a cable connection to the hull, and occasionally had to be "unwound".) Fig. 26E8 on this Web page shows the director in considerable detail. The explanatory drawings of the system show how it works, but are wildly different in physical appearance from the actual internal mechanisms, perhaps intentionally so. However, it omits any significant description of the mechanism of the linkage computer.That chapter is an excellent detailed reference that explains much of the system's design, which is quite ingenious and forward-thinking in several respects.

In the 1968 upgrade to the USS New Jersey for service off Vietnam, three Mark 56 Gun Fire Control Systems were installed. Two on either side just forward of the aft stack, and one between the aft mast and the aft Mk 38 Director tower. [23] This increased New Jersey's anti-aircraft capability, because the Mk 56 system could track and shoot at faster planes.

2. 6. MK 68 Gun Fire Control System (GFCS)

5 inch Mark 42 gun turret

Introduced in the early 1950s, the MK 68 was an upgrade from the MK 37 effective against air and surface targets. It combined a manned topside director, a conical scan acquisition and tracking radar, an analog computer to compute ballistics solutions, and a gyro stabilization unit. The gun director was mounted in a large yoke, and the whole director was stabilized in crosslevel (the yoke's pivot axis). That axis was in a vertical plane that included the line of sight.

At least in 1958, the computer was the Mk. 47, an hybrid electronic/electromechanical system. Somewhat akin to the Mk. 1A, it had electrical high-precision resolvers instead of the mechanical one of earlier machines, and multiplied with precision linear potentiometers. However, it still had disc/roller integrators as well as shafting to interconnect the mechanical elements. Whereas access to much of the Mk. 1A required time-consuming and careful disassembly (think days in some instances, and possibly a week to gain access to deeply buried mechanisms), the Mark 47 was built on thick support plates mounted behind the front panels on slides that permitted its six major sections to be pulled out of its housing for easy access to any of its parts. (The sections, when pulled out, moved fore and aft; they were heavy, not counterbalanced. Typically, a ship rolls through a much larger angle than it pitches.) The Mk. 47 probably had 3-D cams for ballistics, but information on it appears very difficult to obtain.

Mechanical connections between major sections were via shafts in the extreme rear, with couplings permitting disconnection without any attention, and probably relief springs to aid re-engagement. One might think that rotating an output shaft by hand in a pulled-out section would misalign the computer, but the type of data transmission of all such shafts did not represent magnitude; only the incremental rotation of such shafts conveyed data, and it was summed by differentials at the receiving end. One such kind of quantity is the output from the roller of a mechanical integrator; the position of the roller at any given time is immaterial; it is only the incrementing and decrementing that counts.

Whereas the Mk. 1/1A computations for the stabilizing component of gun orders had to be approximations, they were theoretically exact in the Mk. 47 computer, computed by an electrical resolver chain.

The design of the computer was based on a re-thinking of the fire control problem; it was regarded quite differently.

Production of this system lasted for over 25 years. A digital upgrade was available from 1975 to 1985, and it was in service into the 2000s. The digital upgrade was evolved for use in the Arleigh Burke class of destroyers. [24]

AN/SPG-53

Mark 68 GFCS director with AN/SPG-53 radar antenna on top.

Country of origin

United States

Type

Gun fire-control

Precision

Fire control quality, three dimensional data

The AN/SPG-53 was a United States Navy gun fire-control radar used in conjunction with the Mark 68 gun fire-control system. It was used with the 5"/54 caliber Mark 42 gun system aboard Belknap-class cruisers, Mitscher-class destroyers, Forrest Sherman-class destroyers, Farragut-class destroyers, Charles F. Adams-class destroyers, Knox-class frigates as well as others.

2. 7. MK 86 Gun Fire Control System (GFCS)

Mk 45 lightweight gun turret

The US Navy desired a digital gun fire-control system in 1961 for more accurate shore bombardment. Lockheed Electronics produced a prototype with AN/SPQ-9 radar fire control in 1965. An air defense requirement delayed production with the AN/SPG-60 until 1971. The Mk 86 did not enter service until when the USS California nuclear powered missile cruiser was commissioned in February 1974, and subsequently installed on US cruisers and amphibious assault ships. The last US ship to receive the system was commissioned in July 1994. [25]

The Mk 86 on AEGIS class ships controls the ship’s 5"/54 caliber Mk 45 gun mounts, and can engage up to two targets at a time. It also uses a Remote Optical Sighting system which uses a TV camera with a telephoto zoom lens mounted on the mast and each of the illuminating radars.

2. 8. MK 34 Gun Weapon System (GWS)

The MK 34 Gun Weapon System is an integral part of the Aegis combat weapon system on Arleigh Burke-class guided missile destroyers, the only operational class of destroyers in the US. It combines the MK 45 5"/54 Caliber Gun Mount, MK 46 MOD 0 Optical Sight System and the MK 160 Mod 4 Gunfire Control System / Gun Computer System. It can be used against surface ship and close hostile aircraft, and as Naval Gunfire Support (NGFS) against shore targets. [26]

2. 9. MK 92 Fire Control System (FCS)

Mk 75 gun

The Mark 92 fire control system, an Americanized version of the WM-25 system designed in The Netherlands, was approved for service use in 1975. It is deployed onboard the relatively small and austere Oliver Hazard Perry-class frigates to control the MK 75 Naval Gun and the MK 13 Guided Missile Launching System (missiles have since been removed since retirement of its version of the Standard missile). The Mod 1 system used in PHMs (retired) and the US Coast Guard's WMEC and WHEC ships can track one air or surface target using the monopulse tracker and two surface or shore targets. FFG 7 class frigates with the Mod 2 system can track an additional air or surface target using the Separate Track Illuminating Radar (STIR). [27]

2. 10. Mk 110 57 mm gun

The Mk 110 57 mm gun is the newest multi-purpose, medium caliber gun. It's based on the Bofors 57 Mk 3. Compared to WWII destroyers or escorts fitted with 2 or 5 five-inch guns which could fire 15 rounds per minute per barrel, the single Mk 110 can fire salvos at up to 220 rounds per minute, up to a similar range of nine miles with minimal manpower in a turret with a stealthy radar signature. Linked to a digital fire control system, servo-controlled electro hydraulic gun laying subsystems provide extreme pointing accuracy, even in heavy seas. Current and proposed mountings for the weapon include the United States Coast Guard's National Security Cutter, the upcoming Zumwalt class destroyer (close-in), and the new Littoral combat ships. [28]

To increase lethality and flexibility, the ammunition comes equipped a smart programmable fuze with six modes: contact, delay, time, and 3 proximity modes.

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Infantry Tank Mark III Valentine

Posted on December 08 2009 at 04:07 AM

The last British infantry tank to enter production before World War II was the Infantry Tank Mark III “Valentine.” It took its name from the fact that Vickers submitted the design to the War Office just prior to St. Valentine’s Day in February 1938. The chief objection to the new design was the small turret, with space for only two men. In June 1939, however, as war loomed, the government placed an order for 275 Valentines without even a prototype. The first tank was delivered in May 1940. Because of a shortage of cruiser tanks, Valentines served in that role in British armored divisions. They entered the fighting in North Africa in June 1941 and were a staple of fighting thereafter. The Mark I Valentine weighed some 39,000 pounds, had a crew of three, a 135-hp engine, and top speed of 15 mph. It was armed with a 2-pounder main gun and coaxial machine gun and had maximum 65mm armor protection.

The Valentine was a stable gun platform and mechanically reliable. It underwent constant upgrades during the war, including upgunning to a 6-pounder, a more powerful engine, and the addition of long-range fuel tanks. The Valentine was one of the most important British tanks of World War II. A total of 8,275 were built through early 1944, 1,420 of which were manufactured in Canada (all but 30 of these were shipped to the Soviet Union). Valentines also appeared in a wide variety of special purpose AFVs.

Production dates: May 1940–1944

Number produced: 8,275

Manufacturer: Vickers Armstrong; Canadian Pacific (Montreal) produced 1,420, beginning with Valentine VI (all but 30 of these, retained for training, were delivered to the Soviet Union)

Crew: 3–4 (commander, gunner, driver; loader on Mks III and V)

Armament: 1 x 2-pounder (40mm) ROQF Mk. IX or X; 1 x 7.92mm Besa machine gun (coaxial) (Valentine VIII, IX, X mounted a 6-pounder/57mm in place of the 2-pounder; Valentine XI mounted a 75mm gun)

Weight: 39,000 lbs. (41,000 lbs. in Mks VIII–XI)

Length: 17’9”

Width: 8’8”

Height: 7’6”

Armor: maximum 65mm; minimum 8mm

Ammunition storage and type: 79 x 2-pounder; 3,150 x 7.92mm (53 rounds in 6-pounder Valentine VIII, IX, and X; with 1,575 x 7.92mm)

Power plant: AEC six-cylinder 135-hp engine; Valentine II, AEC 131-hp diesel

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Recommended Website: PALO ALTO BATTLEFIELD

Posted on December 08 2009 at 01:47 AM

A Thunder of Cannon

Archeology of the Mexican-American War Battlefield of Palo Alto

CHAPTER FOUR

WEAPONS, ACCOUTERMENTS AND THE SOLDIER


The Mexican-American War transpired at a time when many armies of the world were phasing out their flintlock muskets in favor of more advanced percussion weapons. The flintlock ignition system operated on the principle that sparks result when a sharp piece of flint strikes steel. On a flintlock musket, the jaws of the cock gripped the flint, the latter partly padded with a leather or lead patch to secure the grip. With the pull of the trigger, the flint struck a hardened steel frizzen. The frizzen then pivoted forward, allowing the sparks to fall into a small pan of gunpowder. The powder burned, transmitting a spark through a small hole in the gun barrel and into the main powder charge, thus firing the weapon. The discharged projectile was a large lead ball that killed, or tore a gaping, ghastly wound, if it hit an enemy.

Loading and firing a flintlock musket was slow. Holding the weapon horizontally, the soldier pulled the cock back to half-cock and tipped the frizzen forward to expose the pan. He then drew out a cartridge from his cartridge box. The paper cartridge contained a measured amount of gunpowder, a round lead ball slightly smaller than the inside diameter of the gun barrel, usually weighing about one ounce, and often with two or three smaller lead balls, or buckshot, termed a "buck-and-ball" cartridge. The shooter then tore the end of the cartridge open with his teeth and poured a small amount of powder into the pan and closed the frizzen over it. The remainder of the powder was then poured down the barrel, followed by the lead balls and cartridge paper used as wadding, all of which was then seated firmly onto the powder with the ramrod. The flintlock could then be cocked for firing. The entire process required as many as 17 motions, but a trained soldier armed with a flintlock musket could get off two to three rounds a minute if he did not become rattled in the din of battle.

A percussion musket was simpler to load. The soldier poured all of the cartridge powder into the barrel, and then rammed home the lead balls. Then he pulled the cock, or hammer, to half-cock. He placed a small copper or brass cup-shaped percussion cap on the cone, or nipple, and loading was complete. To fire, one simply cocked the hammer and pulled the trigger. The hammer fell onto the nipple, exploding a small charge of fulminate of mercury in the percussion cap, sending a spark through the nipple and into the main charge.

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Sherman Tank - The War Winner

Posted on December 08 2009 at 01:46 AM

The Sherman tank was comparatively fast and maneuverable, mechanically reliable, easy to manufacture and service, and produced in many special-purpose variants, whose capabilities differed greatly. It was effective in the infantry support role.

The Sherman performed well against World War II Japanese tanks, Italian tanks, and the German standard tank of the time, the Panzer IV medium series which was a pre-war design. However, the typical Sherman was significantly inferior in both armor and armament to the German Tiger heavy tanks, Panther "medium" (heavy by US standards) and some of the tank destroyers fielded by the Germans in 1944.

The majority of losses of Shermans were not from tanks, but from mines, anti-tank guns, and infantry anti-tank weapons. Although American tanks were less powerful than the heavy German tanks, US armored forces won because of numerical superiority and superior combined arms tactics, with Allied air superiority being the biggest danger to the lines of supply for German tank units.

The anecdotes from Allied tank crewmen about the inferiority of the Shermans to late model German tanks has to be balanced against other considerations. Firstly, the Germans were invariably fighting defensively, usually from prepared positions—which tended to made tank casualties disproportionate. On rare occasions when German armored forces had to move against Allied prepared defenses, the Germans had similar complaints. Secondly, there is only so much capability that can be built into a tank of a particular weight; the Pzkw V and the Tiger were larger and heavier (at 42 tons and 56 tons) than the 32 ton Sherman. Finally, the Sherman could be built, deployed, maintained and repaired in large numbers balancing out the tactical advantages of the better German tanks.

According to Belton Cooper's memoir of his 3rd Armored Division service, the Shermans were "death traps"; the overall combat losses of the division were extremely high. The division was nominally assigned 232 Sherman medium tanks; 648 Sherman tanks were totally destroyed in combat, and a further 1,100 needed repair, of which nearly 700 were as a result of combat. According to Cooper, the 3rd Armored therefore lost 1,348 medium tanks in combat, a loss rate of over 580%, in the space of about ten months. Cooper was the junior officer placed in charge of retrieving damaged and destroyed tanks. As such, he had an intimate knowledge of the actual numbers of tanks damaged and destroyed, the types of damage they sustained, and the kinds of repairs that were made. His figures are comparable to those given in the Operational History of 12th U.S. Army Group: Ordnance Section Annex. Some World War II Army officers made similar arguments during the war. Other officers disagreed with the negative assessment and Gen. George S. Patton argued that the Sherman tank was overall a superior tool of war. One of Cooper's other major points in his book, that Gen. Patton was primarily responsible for blocking development of the M-26 Pershing tank, is unsupported by historical facts; Patton did not have the authority to make such decisions - it was Gen. Lesley McNair who opposed the M26.

The only other Second World War tank produced in comparable numbers to the Sherman was the Soviet T-34 series. The Soviets used some Shermans to supplement their own T-34s while Shermans would be pitted against T-34s in Korea. The later 76 mm versions had superior anti-tank power capabilities to the Soviet 85 mm. The T-34's advantages were its low profile, wide tracks which made crossing muddy terrain easier, speed and superior mobility to the Sherman. Both tanks excelled in reliability. Though the Sherman was the final evolution of its design family, while the T-34 would form the basis for postwar Soviet tanks, each was a medium design that served as the primary battlefield tank of its respective country in World War II, was upgraded, served into the Cold War, and outfitted allies.

Walkarounds

"Tanks are Mighty Fine Things"

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MARDER III

Posted on December 05 2009 at 11:25 PM

Marder III Ausf H: H is for "heckmotor" (rear mounted engine)
Marder III Ausf M: M is for "mitte" (middle mounted engine)


There were two self-propelled guns that were known as the Marder III, and both used the same chassis, a derivation of the Skoda TNHP-S tank chassis. This tank had originally been produced by the Skoda factory at Pilsen for the Czech army, but with the annexation of the Czech state by Germany in 1939 the Skoda works continued production of tanks under the designation PzKpfw 38(t) for the German army. The Germans introduced many production and in-service changes to the original Skoda design, and by 1941 the PzKpfw 38(t) may be regarded as a German design, but the original turret was too small to carry weapons powerful enough to defeat enemy armour after 1941, and the chassis was then kept in production for a number of alternative purposes.

One of these purposes came to light in 1941. The appearance of tanks such as the Soviet T-34 meant for a while that the German army had no anti-tank gun powerful enough to knock them out and all manner of hasty improvisations were made to counter this state of affairs, One was to take the chassis of the PzKpfw 38(t) and mount on it a captured Soviet field gun, the 76.2-mm (3- in) Model 1936. This was a very good dual-purpose weapon that could be used as an anti-tank weapon, and the Germans even went to the length of converting some for use as specialized anti-tank guns. On the PzKpfw 38(t) the gun was mounted in a fixed shield and the conversion went into production in early 1942 as the Marder III, otherwise the Panzerjäger 38(t) für 7.62-cm Pak 36(r). Some 344 of these conversions were made, and the Marder III was used not only on the Eastern Front but in North Africa and elsewhere. However, it was at the time regarded only as a stopgap until sufficient numbers of the German 7.5-cm (2.95-m) Pak 40 became available. When this happened during 1942 production of the Soviet-gunned Marder III ceased and that of the German-gunned version commenced. The gun/chassis combination was still called the Marder III, but had the designation Panzerjäger 38(t) Ausf H für 7.5-cm Pak 40/3 and used a slightly differing gun shield and mounting from the earlier model. The first of the Pak 40-armed Marder Ills were rushed into action during the last stages of the Tunisian campaign where some were captured, providing Allied intelligence staffs with something to mull over. But their 'find' did not last for long, for the Marder III was soon to undergo another transformation.

Up to 1943 the various German selfpropelled guns using the Skoda chassis used the PzKpfw 38(t) tank as a basis. However, with some early conversions (including the original Marder III) the vehicles were nose-heavy, which at times limited mobility. Using the original Czech design as a basis, German engineers now relocated the engine at the front of the chassis and moved the 'working platform' to the rear to produce a specialized selfpropelled gun carrier. As soon as this became available Marder III production changed once more to the new Panzerjäger 38(t) Ausf M für 7.5-cm Pak 40/3 configuration with the gun and its protection mounted at the rear of the vehicle. This provided a much better balanced vehicle and the new chassis was also used to mount a variety of other weapons. The late type of Marder III was manufactured by BMM of Prague, and when production ceased in May 1944 799 had been made. They were used on all fronts.

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T-28 - the first indigenous Soviet medium tank design Part I

Posted on December 05 2009 at 11:20 PM

The first indigenous Soviet medium tank design, the T-28, incorporated multiple turrets and was intended for an independent breakthrough role. Inspired by the Vickers A6 (its suspension was a clear copy) and German Grosstraktor designs, it grew out of the 1932 Red Army mechanization plan and was first produced by the Leningrad Kirov Plant. Intended for an attack role, the T-28 had a central main gun turret and two machine-gun turrets in front and to either side. The T-28 weighed 28,560 pounds, had a six-man crew, and was powered by a 500-hp engine and had a road speed of 23 mph. It had only 30mm maximum armor protection. The prototype mounted a 45mm gun, but production vehicles had a 76.2mm low-velocity main gun and two machine guns. Combat experience with the T-28 led to changes. Armor was increased on the C version to 80mm for the hull front and turret. Some T-28s substituted a low-velocity 45mm gun in the right front turret for the machine gun normally carried there. The T-28 had a poor combat record, however.

Production history

The T-28 was in many ways similar to the British Vickers A1E1 Independent tank. This tank greatly influenced tank design in the period between the wars, although only one prototype was manufactured in 1926. The Kirov Factory in Leningrad began manufacturing a tank, which was based on the British Independent in 1932. The T-28 tank was officially approved on August 11, 1933. The T-28 had one large turret with a 76.2mm gun and two smaller turrets with 7.62mm machine guns. A total of 503 T-28 tanks were manufactured over a period of 8 years from 1933 to 1941.

The type would not have that much success in combat, but it played an important role as a development project for the Soviet designers. A series of new ideas and solutions were tried out on the T-28 and were later incorporated in future models.

Combat history

The T-28 was deployed during the Invasion of Poland and the Winter War against Finland. During the initial stages of the Winter War, the tank was used in direct fire missions against Finnish pillboxes. In the course of these operations it was found that the armour was inadequate and programs were initiated to upgrade it. Frontal plates were upgraded from 50 mm to 80 mm and side and rear plates to 40 mm thickness. With this up-armoured version the Red Army broke through the main Finnish defensive fortification, the vaunted Mannerheim Line.

According to Russian historian M. Kolomietz's new book T-28. Three-headed Stalin's Monster, over 200 T-28s were knocked out during the Winter War, but only 20 of them were in irrecoverable losses (including 2 captured by the Finnish Army). Due to proximity of the Kirov Plant, all other knocked-out tanks were repaired, some of them over five times.

The Finns knew the T-28 as the Postivaunu ("mail wagon" or stagecoach), a name which alluded to Finnish troops' discovery of Red Army field mail sacks inside the first destroyed T-28. Another explanation is that the high profile of the tank resembled the old west stagecoaches of the United States. Finns captured two T-28s during the Winter War and five in Continuation War, totalling 7 vehicles.

The Soviets had 411 T-28 tanks when the Germans invaded in June 1941. Most T-28s were lost during the first two months of the invasion, many of them abandoned after mechanical breakdown. Some T-28s took part in the 1941 winter defence of Leningrad and Moscow, but after late 1941, they were rare in Red Army service; a few were operated by enemy forces.

Today three T-28s remain, two in Finland and one in Moscow. One restored T-28 is on display in Finnish field camouflage in the Parola Tank Museum, Finland.

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T-28 - the first indigenous Soviet medium tank design Part II

Posted on December 05 2009 at 11:20 PM

Summary

First indigenous Soviet medium tank, but clearly influenced by both the Vickers A6 and German Grosstraktor designs. Intended for an attack role, it had a central main-gun turret and two machine-gun turrets in front to either side. Its suspension was copied from the Vickers tank. It served in the 1939–1940 Winter War with Finland and in the opening weeks of the German invasion of the Soviet Union in June 1941 but performed poorly in combat. Subsequent variants included the T-28C with increased hull front and turret armor.

Evaluation

Although the T-28 was rightly considered ineffective by 1941, it is worth remembering that when the Red Army was fielding the first T-28s in 1933, the French Army was still largely equipped with the FT-17, and the Reichswehr had no tanks at all. No army had a series-production medium tank comparable to the T-28 for several years.

The T-28 had a number of advanced features for the time, including radio (in all tanks) and anti-aircraft machine-gun mounts. Just before the Second World War, many received armor upgrades, bringing its performance on par with the early Panzer IV, although its suspension and layout were outdated. [5]

The T-28 had significant flaws. The plunger-spring type suspension was poor, but many of the better suspension designs used in World War II tanks had not yet been developed. The engine and transmission were troublesome. Worst of all, the design was not flexible. Although the T-28 and early PzKpfw IV were comparable in armour and firepower, the good basic design of the PzKpfw-IV allowed it to be significantly upgraded, while the T-28 was a poor basis for improvement.

Unfortunately for the Red Army, by the time the T-28 saw combat in 1939, events had overtaken it. The 1930s saw the development of the first reliable high-speed suspensions, the first purpose-designed antitank guns, and a gradual increase in the firepower of tanks. The Spanish Civil War showed that infantry units with small, towed anti-tank guns could defeat most contemporary tanks, and made the under-armoured tanks from the early 1930s particularly vulnerable.

Despite heavy losses, in the Winter War the Red Army's 20th Tank Brigade, equipped with T-28s, fulfilled its mission to break the defensive Mannerheim Line. As an infantry-support tank, designed to support infantry in breakthrough operations, the T-28 in general was successful for an early 1930s design.

Variants

  • T-28 Model 1934 or T-28A — main production model with the same machinegun turrets, and similar main turret as the T-35 heavy tank and Model 27/32 76.2mm gun.
  • T-28 Model 1938 or T-28B — version with improved L-10 76.2 mm gun (from 16.5 calibres to 26 calibres), improved gun stabilization system and improved Model M-17L engine.
  • T-28E or T-28C — 1940 addition of appliqué armour in response to poor performance in Finland. Total front armour was increased to 80 mm, weight to 32 t, and road speed dropped to 23 km/h
  • T-28 Model 1940 — the final batch of about twelve tanks had the same conical turret as late-production T-35 tanks.
  • OT-28 — flamethrower version.

Experimental models

Several self-propelled guns, the IT-28 bridging tank, and an engineering vehicle with mine rollers were tested on the T-28 tank chassis, but none was accepted for production. The T-29 was a prototype medium tank, a modernized T-28 with Christie suspension — a later version of this vehicle was considered for the competition of prototypes which led to the T-34, but by then it was outdated (not to be confused with a Grotte tank project also called T-29). The T-28 also served as a testbed for the KV tank suspension.

Production dates: 1933–1940

Number produced: 503

Manufacturer: Leningrad Korov Plant

Crew: 6

Armament: 1 x 76.2mm (3-inch) low-velocity main gun M1927; 3 x 7.62mm DT machine guns (some T-28s mounted a low-velocity 45mm gun in the right auxiliary turret in place of the machine gun)

Weight: 62,720 lbs.

Length: 24’5”

Width: 9’5”

Height: 9’3”

Armor: maximum 30mm; minimum 10mm (maximum 80mm on T-28C)

Power plant: M-17 V-12 500-hp gasoline engine

Maximum speed: 23 mph

Range: 137 miles

Vertical obstacle: 3’5”

Trench crossing: 9’6”

Special models: commander’s tank T-28 (V) with radio antenna frame around turret; small number of flamethrower tanks

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Sukhoi Su-22M4 Fitter-K

Posted on December 05 2009 at 11:19 PM

This powerful Russian-designed ground attack aircraft was a versatile weapon in the Soviet Union's air forces for many years, and it was one of the Soviets' first variable geometry or "swing-wing" attack aircraft. Variable geometry wings allow aircraft to adjust speed, lift and maneuverability characteristics in flight and to operate from short airfields. The swing-wing aircraft series designated "Fitter" by NATO began with the Su-7 Fitter-A fighter-bomber, a fixed-wing fighter that entered Soviet service in 1959. In the late 1960s, when Western and Soviet aircraft designers began developing swing-wing aircraft, Sukhoi installed variable wings and a more powerful engine in the Fitter. This alteration greatly improved the airplane's performance, and NATO designated it the Fitter-B.

Several updated versions followed, with improved engines, radars, weapons, and airframes. Western analysts first identified Fitter-Ks, like the one on display, in 1984. Produced until 1991, Fitters could carry a large variety of weapons and stores, and were exported to nations such as Iraq, Afghanistan, Syria, Poland and several others.

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The SU-22M4 is one of the last variants from a long line of fighter bombers that started with the SU-7, even the interceptors SU-9, 11 and 15 share the same roots.

This aircraft, originally the soviet SU-17 (first flown in 1966), was the first plane of this family to feature variable wing geometry. The mostly simplified export variants were designated SU-20 and SU-22 and further development lead to sub-variants such as the SU-22M4. NATO-Code for all versions is “Fitter” with an annex letter to distinguish the different types.

The SU-22 became famous in 1981, when two Libyan SU-22M3’s found out the hard way that the US Navy also operated swing-wing fighters that are better not to be messed with.

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Polish Air Force Su-22 Fitters at Istrana

After previous year's squadron exchange, which was the first between the Areonautica Militare Italiana (AMI - Italian Air Force) and the Sily Powietrzne (Polish Air Force), 2007 saw the Polish Fitters again operating from an Italian air base. This time it was Istrana AB, home of the 51° Stormo hosting the 103° and 132° Gruppo. Both squadrons are equipped with the AMX.

From June 29th until July 12th three Su-22M4 single-seaters and one Su-22UM3K two-seaters from 7 ELT (7 Eskadry Lotnictwa Taktyczego - 7th Tactical Fighter Squadron) operated together with both the 103° and 132° Gruppo flying operational training missions such as DACT (Dissimilar Air Combat Training) and CAS (Close Air Support), in support of integration of NATO standards in the Polish Air Force. Two missions were flown daily, one in the morning and one in the afternoon.

During the squadron exchange one of the Polish pilots reached 1,000 hours flying the Su-22 and a little “shower” awaited him on his return to base.

The 7 ELT is based at Powidz and is equipped with single-seat Su-22M4 'Fitter-K' and two-seat SU-22UM3K 'Fitter-G' conversion trainers. Some of the former 6 ELT Su-22s are still flown by 7 ELT, retaining the old 6 ELT badge on fin as the seen on the two-seater. 6 ELT is currently undergoing conversion to the new F-16C/D Block 52+ having moved to Poznan-Krzesiny AB. The 'Fitters' are scheduled to fly until 2010-2012 and then the unit will become a transport squadron flying the C-130 Hercules.

TECHNICAL NOTES:
Crew:
One

Armament: 9,370 lbs. of various nuclear weapons, bombs, rockets, missiles and gun pods on eight external pylons

Engine: Lyul'ka AL-21F-3 turbojet of 24,700 lbs. thrust with afterburner

Maximum speed: 1,550 mph (Mach 2.09)

Wing sweep: Variable in three fixed positions: 28 degrees for low speed and 62 degrees for high speed, plus one intermediate position


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Dassault Mirage III

Posted on December 04 2009 at 03:33 PM


Type: Fighter; Light Bomber

Dimensions: wingspan, 26 feet, 11 inches; length, 49 feet, 3 inches; height, 14 feet, 9 inches

Weights: empty, 15,542 pounds; gross, 21,164 pounds

Power plant: 1 × 9,436–pound thrust SNECMA Atar 9C-3 turbojet engine

Performance: maximum speed, 1,460 miles per hour; ceiling, 75,460 feet; range, 746 miles

Armament: 2 × 30mm cannons; up to 8,818 pounds of bombs or rockets

Service dates: 1961–

The sleek Mirage III remains one of the classic fighter designs of all time and helped propel France to the forefront of military aviation. Through constant upgrades, many still fly in frontline service around the world.

In 1952 the Armee de l’Air sought an advanced lightweight interceptor to replace its aging Dassault Mysteres. The desired craft was intended to be built around two small turbojets and a small rocket booster. Dassault complied with a small delta design, the Mirage I, in 1953, but it was rejected as insufficiently powered. The firm then went on to develop the bigger Mirage III as a company project; it was powered by a single turbojet engine. In 1956 this craft became the first European warplane to exceed Mach 2, and the French military immediately expressed interest. The Mirage III was a conventional delta design, with a relatively small wing and a sharp, pointed profile. It was highly maneuverable and handled well, but like all delta designs it suffered from high landing speeds and a prolonged takeoff. Nonetheless, the first Mirage III entered service in 1961 and was followed by numerous multimission variants. It was also widely exported abroad, especially to Israel, which used them with decisive effect in the 1967 war. Most French machines have since been retired, but Mirage IIIs are continually upgraded and flown by several air forces, including Australia, Argentina, Brazil, and South Africa.

In 1967 Israel asked Dassault to design a cheaper ground-attack version, which subsequently emerged as the Mirage 5. This model lacked advanced radar systems in exchange for more fuel and greater payload. It too was an export success. The final development was the Mirage 50 of 1979, which utilizes the Mirage 5 airframe in concert with a more powerful engine and advanced avionics. It is currently utilized by more than 20 nations and will continue flying well into the twenty-first century. A total of 1,400 Mirages of all variants has been constructed.


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Gribeauval 8-pounders for Horse Artillery

Posted on December 04 2009 at 03:32 PM

There were improvements in artillery during the Napoleonic Period. Guns became more mobile and accurate, developments pioneered in Austria and Prussia, and introduced into the French service by de Gribeauval. Gribeauval artillery was provided with an elevating screw mechanism and calibrated tangent rear sights, considered the most significant improvements in the design of ordnance during the last two hundred years of the smoothbore era. While historians have made much of the supposed uniqueness of his range of field guns - 4-pounders (1.8 kg), 8-pounders (3.6 kg) and 12-pounders (5.4 kg) - Austrian, Prussian and English artillery was nearly as hard-hitting and mobile as the French, and was often utilized when captured.

In 1793 Gaspard Monge, the distinguished mathematician and scientist in charge of artillery procurement, estimated France was 6,000 pieces of artillery short. To speed up production Monge invented a simplified casting method, built furnaces in converted churches and trained additional workmen. Copper for the bronze barrels was obtained by requisitioning church bells and through tacit trade with the enemy: Production expanded during the Consulate and the Empire and seventeen new foundries turned out an astonishing quantity, yet supply never caught up with demand even though much captured materiel was pressed into service. Although the Austrian ordnance was slightly outmatched by their French equivalents in throw weight, Napoleon was well impressed and used it widely: At Wagram about one-third of his artillery was of Austrian origin, while light Prussian cannons were widely issued in Spain.

Gribeauval System Field Guns

Field guns included 4-, 8-, and 12-pounders, and Gribeauval at last incorporated new 6-inch howitzers into the French army as regulation field weapons. The 8-inch howitzer already in service since 1749 was also retained but was used on a more limited basis. The earliest Gribeauval field howitzer was heavily based on Prussian models that he had studied, but his later designs were so modified that they were virtually an entirely new type.

Gribeauval also redesigned his gun carriages so as to be more durable than the Austrian Lichtenstein models, to compensate for the combined rear and downward recoil—an improvement that both strengthened their construction and produced a lighter and shorter carriage than earlier models. Carriages were originally painted various shades of blue until after the Revolution, when their color was changed to green. Field carriages were also improved by the addition of black-painted iron reinforcing straps to stress points in the woodwork as well as the leading edges exposed to damage. A coffret—a removable ammunition chest located between the flasks—enhanced the ability of the crews to more quickly put their pieces in action during combat. To improve balance and enhance the stability of the guns while on extended marches, Gribeauval, borrowing from Lichtenstein’s 12-pounder carriage, added an extra pair of half-round trunnion cutouts toward the rear of the carriage. This feature, known as encastrement, did, however, require a rather laborious process involving levering and rolling with two handspikes to move the tube between the two positions. It was thus rarely if ever used in situations where combat was imminent.

Transportation was further improved with the introduction of a more efficient limber mounting a pole for the hitching of horses in side-by-side pairs. For transport, the reinforced hole in the transom at the end of the trail was passed over a pintle mounted over the limber’s axle and secured to make a four-wheeled cart. A four- horse team was required for the 4- and 8-pounders, and six horses for the 12-pounders. Gribeauval also introduced the caisson, essentially a large, four-wheeled ammunition chest with a rounded or peaked lid and a compartmentalized interior for various types of ammunition and equipment. The combination of the new limber and caisson enabled French field gunners to arrive on the field with their ammunition and thus go into action more rapidly than their opponents.

Gribeauval’s method of elevating his field guns’ tubes was also somewhat different from that of other European systems. Although employing a vertical elevating screw, as did most other contemporary systems, his screw did not come into direct contact with the barrel’s breech. It instead pushed against a wooden platform hinged to a transom beneath the barrel. Howitzers’ trunnions remained below the centerline, as they had in the Vallière System, but they too differed in their aiming mechanism. Although still retaining a quoin, it was adjusted mechanically for elevation by way of a horizontally mounted screw attached to the transom beneath the breech.

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Soviet Aircraft Experimental Landing Gears

Posted on December 04 2009 at 03:26 AM

No country has as much real estate as the former Soviet Union, and the land surface is at times soft mud, sand, snow and hard frozen. Several designers concentrated on devising landing gears that would enable aircraft to operate from almost any surface. One of the first was N A Chechubalin, who in the 1930s was working at BRIZe, a division of Glavsevmorput', the chief administration of northern (Arctic) sea routes. He devised neat tracked main gears to spread the load and enable aircraft to operate from extraordinarily soft surfaces. His experimental gears were tested on a U-2 and a much heavier Polikarpov R-5.

In 1943 S A Mostovoi picked up where Chechubalin had left off and designed caterpillar main landing gears for an Li-2 transport (the Soviet derivative of the DC-3) These gears were retractable, and made little difference to the performance of the aircraft, but they were 'unreliable in operation' and were therefore not put into production. Photographs have not yet been found.

In 1937 Nikolai Ivanovich Yefremov collaborated with Aleksandr Davidovich Nadiradze to design a unique inflatable gear which offered a totally different way of reducing footprint pressure in order to operate from almost any surface. Their answer was an 'air pillow' inflated under a semi-rigid upper sheet attached under the aircraft centreline. The scheme was called SEN, from the Russian for 'Aircraft Yefremov/Nadiradze'. The pillow was tested on a Yakovlev AIR-20 (UT-2), which was fitted with a 20hp motorcycle engine driving a compressor to keep the bag inflated. The only known photo does not show the wingtips clearly, so it is not known if wingtip skids were needed to stop the aircraft rolling over. In 1940 the SEN was test-flown by such famous pilots as Gromov, Shelest and Yumashev, but it never went into general use.

In 1991 the new private company Aeroric, at Nizhny Novgorod (in Communist days called Gorkii), began the design of a multirole transport called Dingo. Powered by a 1,100-shp Pratt & Whitney Canada PT6A-65B turboprop, driving a Hartzell five-blade pusher propeller, the Dingo is made mainly of light alloy and accommodates one or two pilots and up to eight passengers or up to 850kg (1,8741b) of cargo. Its most unusual feature is that it has no conventional landing gear. Instead it has a 250hp Kaluga TBA-200 (in effect a turbofan) which generates an air cushion underneath, contained by inflated air bladders along each side and hinged flaps at front and rear. At full load the ground pressure is a mere 0.035kg/cm2 (71.71b/ft2), enabling the Dingo to ride over water, snow or any other surface and to cross ditches, ledges and projections up to 30cm (1ft) high. Cruising speed is275km/h(170mph).

Though a surface skimmer rather than an aeroplane, the Stela M.52 seen at the 1995 Zhukovskii airshow was interesting for riding on an air cushion. This is contained by side skegs (underfins), a large rear flap and front hinged curtains.

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Hitler's Superpanzer Dud!

Posted on December 03 2009 at 03:41 AM

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Turan

Posted on December 01 2009 at 06:55 PM

Medium tank based on the Czech Skoda S-2r medium design of 1937, produced under license with the Germans after their takeover of Czechoslovakia. The Turan utilized a modified Vickers bogie suspension with eight road wheels in four pairs per side. The turret was enlarged to hold three, a Hungarian manufactured 40mm main gun, and a more powerful engine. The Turan I formed the chief equipment of the Hungarian 1st Tank Division from 1943. The Turan II was essentially an upgunned Turan I with a short 75mm gun. Manufacture ended in 1944 when the Hungarian Army adopted the PzKpfw III and IV tanks.

By J.C.M. Probst

DESPITE the minimal interest hitherto bestowed upon the Hungarian Turan Tank by AFV historians, this vehicle served as the main battle tank of Hungarian armoured divisions in the latter part of World War 2 and was used in quite considerable numbers. The Turan tanks and their assault howitzer derivation, the Zrinyi vehicls, bore the brunt of the fighting of the Hungarian armoured forces in the fatal year 1944.

SKODA LICENSE

In 1939 Hungary looked for a medium tank suitable for licensing. In the Czech Army’s 1938 trials for a medium tank there had been two contenders, the CKD (Praga) V-8-H and the Skoda S-3. Since the V-8-H was selected by the Czech Army as their ST-39 medium tank, the Skoda designers began working on another construction, the S-IIc, which they developed from their LT-35 light tank (Skoda S-IIa) for export applications. The S-IIc was offered to Hungary by Skoda, and the V-8-H was offered by CKD.

In 1940 the designation S-IIc was changed into Skoda T-21 and an improved and up-armoured version, the T-22, was made. The T-22 was shown to a Hungarian commission in Pilsen in May 1940, and it was demonstrated in Hungary during June and July. The V-8-H was also evaluated, but a licensing agreement was signed for the T-22 medium tank in August.

Before production, the Czech tank was modified on a number of points: a three-man turret was substituted for the original two-man version, and a 260hp V-8 engine designed by the Hungarian company Manfred Weisz was installed. Armament was of Hungarian design as well. The new tank was dubbed Turan.

THE 40mm 41M L/51 TANK

A special tank-mounted version of the standard Hungarian 40mm 40M towed antitank gun (derived from the German Rheinmetall-Borsig 3.7cm Pak 35/36, which was used by Hungarian troops as the 37mm 36M antitank gun) was developed by MAVAG. In addition, in November 1940 a license was obtained for the Skoda 40mm Type A17 tank gun developed from the A7 gun used in LT-38 tanks. It appears that the tank mount of this gun was mated to the Hungarian 40mm 40M gun and the result was the 40mm 41M tank gun of the Turan tank.

This gun fired the same ammunition as the 40mm 37M Bofors antiaircraft gun, which was also made by MAVAG. 101 rounds of ammunition were carried by the Turan.

Machine-guns were the 8mm 34/40M air-cooled belt-fed tank machinegun derived from the Czech Brno ZB30 and made under license by Danuvia.

The first prototype of the Turan tank was finished by August 1941 and production was started in October. The Hungarian service designation of the tank was 40M Turan I medium tank (kozepes harckocsi), which in 1944 was changed into 40M Turan 40 medium tank.

The name Turan comes from Hungarian prehistoric legend, according to which the Turans were an ancient Asian people, from which the Hungarian people originated.

TURAN I PRODUCTION

An initial order of 190, later raised to 230 tanks, was placed by the Hungarian government in October 1941, and 70 tanks were built by Manfred Weisz of Csepel, 50 at Ganz of Budapest, 70 at MVG of Cyor and 40 at MAVAG of Budapest. Guns were produced at MAVAG Diosgyor and likewise most other components for these vehicles were produced by Hungarian industry.

The initial order was followed by a new order in 1942 for 70 tanks, of which 24 were eventually built by Ganz, 12 by MVG and 19 by MAVAG Budapest.

With deliveries to the troops starting in the beginning of 1942, a grand total of 285 Turan I tanks had been produced when war events stopped production in 1944. Of these no less than 242 were delivered during 1942, and only 43 during 1943 & 1944.

Production of the Turan I tanks in 1942 was a major effort by Hungarian industry and the tanks were used to equip the 1st & 2nd Armoured Divisions and the 1st Cavalry Division in 1942-43. However, the disaster of the Hungarian 2nd Army on the Don in January 1943 (where no Turan tanks participated) suddenly made it clear that the Turan I was obsolete compared to Soviet tanks, and that a gun caliber of 75mm was the minimum acceptable for a modern tank.

THE 75mm 41M L/25 TANK GUN

Development of a version of the Turan with a short 75mm gun had started in 1941. It was seen as a heavy support vehicle to supplement the medium Turan I main battle tank in armoured divisions.

The gun was developed by MAVAG from the Austro-Hungarian Bohler 76.5mm 18M field gun, and as the 75mm 41M tank gun it was produced by MAVAG Diosgyor. The gun had some armour-piercing capability but could not stop a Soviet T-34 tank at any reasonable distance. 52 rounds of ammunition could be carried.

The Hungarian service designation of the Turan version with this gun was 41M Turan II heavy tank (nehez harckocsi), which in 1944 was changed into 41M Turan 75 rovid (short) heavy tank. Even with its short gun the Turan II was suddenly the only usable tank available to Hungarian troops in 1943 and it still had to be produced in quantity.

An order for Turan II tanks had been placed in 1942 and the first three Turan II tanks were delivered to troops on May 13th & 15th, 1943.

TURAN II PRODUCTION

A total of 139 Turan II tanks were produced, mainly in 1943 and the beginning of 1944, against a total order of 322, which should have been completed in 1945. Of these 54 were produced by Manfred Weisz of Csepel, 36 by Ganz of Budapest and 39 by MVG of Gyor.

By the middle of August 1943 a total of 49 Turan II tanks had been delivered, and in October another 66. They were allocated to the 2nd Armoured Division and the 1st Cavalry Division, [with] 24 going to the new assault artillery battalions, which needed them as a stopgap until delivery of Zrinyi vehicles. Later the 1st Armoured Division received its share of Turan II tanks as well.

Since no better vehicles were available the Turan II tank became the main battle tank of Hungarian troops in 1943 and it bore the brunt of the fighting of Hungarian armoured troops in 1944.

THE 75mm 43M L/43 TANK GUN

In April 1943 it was decided that a modern tank needed a 75mm long [barreled] antitank gun. MAVAG developed a speical Hungarian version of the German 7.5cm KwK 40 tank gun which fired both standard German and special Hungarian ammunition. This gun, which allegedly differed considerably from the German model, became the 75mm 43M tank gun.

Plans were drawn up that all available Turan tanks should be modernized on the following points from the middle of 1944 onwards:

--- retrofit with a 75mm 43M tank gun

--- additional armour fitted

--- skirt plates fitted

and work on a prototype vehicle was initiated.

In the winter [of] 1943/44 the prototype was completed as the Turan III heavy tank, and was called the 43M Turan hosszu (long) heavy tank from early 1944. It mounted the 75mm 43M gun in a modified turret and had thicker armour, but was otherwise similar to the Turan I and II. It carried 32 rounds of ammunition.

Production of the Turan II or modification of existing Turan tanks was not initiated for political and military reasons and Hungarian AFV production came to an almost complete stop following the German occupation on March 19th, 1944. The modification plan, however, explains the continued Turan I production into 1944.

The only Turan III modifications actually undertaken on existing Turan tanks were the fitting of skirt plates over the suspension and around the turret on some Turan I and II tanks in the second half of 1944. This gave the Turans an appearance very closely resembling the late German PzKpfw III tanks with skirt plates.

THE TURANS IN BATTLE

Hungarian tank regiments of 1944 had an equal number of Turan I & Turan II tanks, even if the Turan I was completely obsolete as a battle tank. Some of the Turan I tanks were equipped as command tanks. These tanks had an R/4T radio set instead of the left side ammunition boxes. They were called 40M Turan I pk medium tanks (pk = parancsnoki = command), and later 40M Turan 40 pk medium tanks. The command tanks were used by battalion and regimental commanders.

All Turan tanks, including the command models, had a R/5a radio set installed for communication to other tanks in the unit.

The Turan tanks were first committed to battle of April 17th, 1944, in Galicia, when the 2nd Armoured Division launched a counterattack from

Solotwina towards Kolomea. This was in a wooded and mountainous terrain with many streams, which were a particular problem because of snow melting at the time. So the terrain was a rather bad choice for a tank attack and the division was stopped in tank-to-tank fighting by small Soviet T-34 forces without reaching Kolomea. The attack was called off on April 26th, 1944. 30Turan I & II tanks were lost; that represented 26 percent of the initial tank strength of the division.

From June to Septmeber 1944 the 1st Cavalry Division with a battalion of Turan I & II tanks fought in eastern Poland and around Warsaw, and from September 1944 onwards this division and the 1st & 2nd Armoured Divisions were engaged in heavy fighting in Hungary proper.

Only very few German tanks were given to Hungarian units in 1944, and since the inferiority of the Turans compared with Russian tanks was well realised by Hungarian commanders, the Hungarian armoured units were committed to battle somewhat reluctantly in the latter half of 1944.


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Russian WWI Naval Air

Posted on December 01 2009 at 06:54 PM

Grigorovich M-5

This aircraft based on the seaplane carrier Imperator Alexander I. Black Sea Fleet.

Grigorovich M-9

Black Sea Fleet.

The other –than the Royal navy - great exponent of carrier aviation during World War I was the Imperial Russian Navy in the Black Sea. From early 1915 the Black Sea Fleet mounted a sustained interdiction campaign against Turkish sea communications. A particular target was the coal trade from Anatolia to Constantinople on which the Turkish- German fleet largely depended and that had to come by sea because there was no rail line and the road system was inadequate. According to Russian claims, their naval forces sank over 1,000 vessels during this campaign, in which the fleet’s aircraft carriers played a central role and must have been directly responsible for an appreciable percentage of these successes. On more than one occasion the battle cruiser Goeben and the light cruiser Breslau, units technically transferred to the Ottoman Navy from the German fleet but actually commanded and manned by Germans, that formed the modern heart of Turkish naval forces were incapable of putting to sea on operations for lack of fuel reserves.

The three carriers converted in early 1915 were fast enough to maintain formation with the older battleships that initially formed the core of the fleet and could keep up with even the new dreadnoughts that joined the fleet later. Consequently, there were few operations of any size in which the carriers were not tightly integrated and in several of those against the Anatolian and Bulgarian coastlines, the carriers formed the principal striking force with the battleships relegated to support and distant cover roles. Russian carriers used Curtiss flying boats initially, which eventually were supplanted by excellent indigenous Grigorivich boats. The carriers carried large numbers of aircraft for the period and their crews were highly trained, so their launch rates were impressive. One American observer timed a carrier launching seven aircraft in fifteen minutes, compared with the Royal Navy’s standard of twenty minutes to launch three aircraft (admittedly under North Sea conditions). After 1916, when Romania joined the war, the Black Sea Fleet’s aircraft carrier strength increased when one Romanian auxiliary, the Rominia, joined the fleet as a full-time carrier and was supplemented periodically by four other auxiliary cruisers embarking aircraft as operationally necessary. The carriers’ aircraft attacked Turkish and Bulgarian ports, their facilities, and ships at dock, conducted widespread reconnaissance missions, raided coastal shipping, bombed shore installations, spotted for the fleet’s guns, and provided cover for mine-laying operations and convoys.

By the end of World War I, naval aviation had secured for itself an important place in operations. For the most part, however, naval aircraft were shore based. While operational experience had confirmed the potential value of carrier-based aviation, the technical and functional details necessary for success remained immature. Major navies accepted that aircraft carriers were an essential feature of future fleets but the shape, size, arrangements, facilities, and equipment all were uncertain and still required much experiment and testing.

RUSSIA: ALMAZ (1915)

Builder: Baltic Works, St. Petersburg

Laid down: September 25, 1902. Launched: June 2, 1903. Commissioned: 1915

Displacement: 3,285 tons (normal)

Dimensions: 363’0” (oa) x 43’6” x 17’6” (mean)

Machinery: Vertical triple-expansion engines, Belleville boilers, 2 shafts, 7,500 ihp = 19 knots

Aircraft: 4

Armament: 7 x 4.7”, 4 x 12 pdr AA

Complement: 340

Design: Originally completed as an armed yacht rated as a third-class cruiser, the Almaz served as the viceregal yacht in the Far East and was the largest Russian survivor of the Battle of Tsushima (May 27-29, 1905). The Almaz was transferred to the Black Sea Fleet in 1911 and refitted as a seaplane carrier early in 1915. Seaplane handling platforms were fitted behind the mainmast and additional booms were rigged for lifting aircraft. Service: The Almaz formed part of the Hydro-Cruiser Division of the Black Sea Fleet from 1915 to 1917. As the fastest of the fleet’s seaplane carriers, it often undertook independent missions, including raids on Varna in Bulgaria in October 1915 and June 1916. After the popular revolution in 1917 the Almaz became a Bolshevik headquarters ship but was seized by French forces at Odessa in December 1918 and turned over to White Russian forces. It sailed to Algiers in 1920 with other White Russian vessels, was taken over there by the French in 1928, and scrapped in 1934.

RUSSIA: CONVERTED MERCHANTMEN (1915)

Builder:

Imperator Nikolai I: John Brown & Company Ltd., Clydebank

Imperator Alexandr I: William Denny & Brothers Ltd., Dumbarton

Displacement: 9,230–9,240 tons (normal)

Dimensions: 381’0” (oa) x 52’0” x 26’0” (mean)

Machinery: Vertical triple-expansion engines, 4 boilers, 2 shafts, 5,100 ihp = 13.5 knots

Aircraft: 8

Armament: 6 x 4.7”, 4 x 12 pdr AA

Complement: Unknown

Design: These two vessels were built as fast cargo liners for the Russian Steam Navigation Trading Company and completed in 1913 and 1914, respectively. They were requisitioned as naval auxiliaries after the outbreak of World War I and converted into seaplane carriers in early 1915. The conversion was minimal, involving fitting additional booms for aircraft handling and clearing after superstructure space to make room for aircraft stowage on the upper deck. Service: These vessels formed the core of the Black Sea Fleet’s Hydro- Cruiser Division and were very active against Turkish and Bulgarian coastal targets from March 1915 to February 1917. After the popular revolution they were renamed the Aviator and the Respublikanetz, but were laid up from April 1917 until they were taken over by French forces in December 1918. Both vessels entered French commercial service after World War I, serving with the Compagnie des Messageries Maritimes as the Pierre Loti and the Lamartine. The Pierre Loti was wrecked in the Gabon River estuary in 1943 and the Lamartine, by then renamed the Khaidinh, was sunk by United States Navy aircraft in Along Bay in 1942.

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Fokker Scourge

Posted on December 01 2009 at 06:53 PM

Fokker E III

In the autumn of 1915, the anachronistic-looking Eindekker reigned as the world’s best fighter aircraft. Its superiority over contemporary French and English machines ushered in a period known as the “Fokker scourge”—and the dawn of modern aerial warfare.

April 19, 1915, signified a turning point in the history of military aviation when the French-built Morane-Saulnier L aircraft piloted by Roland Garros crashed behind German lines. German investigators combing through the wreckage discovered that Garros had clandestinely mounted a machine gun fixed so as to fire through the propeller arc. The propeller itself was fitted with metal wedges to deflect any unsynchronized projectiles, but the Germans recognized the advantages an improved system would bring. The brilliant aircraft designer Anthony Fokker was contacted, whose firm was familiar with the concept, and within two weeks a completely synchronized interrupter gear was devised. This allowed bullets to shoot through a moving propeller by being deliberately timed to miss it. This technology was then grafted onto a Fokker M 5 monoplane, a design that had been flying since 1913, for trials. Thus was born the Fokker E I, the world’s first true fighter craft. A total of 420 of all models were built, and their tactical implication was immense.

At a time when Allied craft were either unarmed or simply carried rifles and other sidearms for defense, the new Fokker Eindekkers represented a quantum leap in firepower. Throughout the fall and winter of 1915, they sawed through nearly 1,000 allied reconnaissance craft, chiefly lumbering British Be 2cs. The Fokkers also stimulated the evolution of new fighter tactics as pioneered by Germans aces like Max Immelmann and Oswald Boelcke. For several months the “Fokker scourge” dominated the skies of Western Europe until the spring of 1916, when superior fighters like the Nieuport 11 Bebe and the de Havilland DH 2 pusher debuted. The days of the ugly, ungainly Eindekkers were numbered in weeks, but a corner had been turned. Hereafter, warplanes ceased being frail-looking contraptions and evolved into machines of increasing deadliness.

Country of origin: Germany

Manufacturer: Fokker Flugzeug-Werke

Type: Fighter

Crew: 1

Dimensions: Wingspan 31 ft 2.75 in.; Length 23 ft 11.3 in.; Height 9 ft 1.75 in.

Loaded weight: 1,400 lbs

Power plant: 1 x 100 hp Oberursel U.I rotary

Performance: 87 mph maximum speed; 3,500 m (11,483 ft) service ceiling; 2 hour 45 minute endurance

Armament: 1 x 7.92 mm fixed forward-firing Synchronized Parabellum or Spandau machine gun

Total production: Approximately 220 of all types service dates: 1915–1916

#

Although Germany had enjoyed some success by using its Albatros C-type armed reconnaissance aircraft to shoot down Allied aircraft, Roland Garros’s demonstration of the advantage of forward fire through the arc of the propeller of his Morane-Saulnier monoplane convinced the Germans of the need to develop an aircraft with similar capabilities. After obtaining access to both Garros’s plane, which had been forced down behind German lines, and Franz Schneider’s prewar patent, Dutch designer Anthony Fokker quickly developed a synchronization gear that worked off the camshaft to interrupt the firing of either a Parabellum or Spandau machine gun. This was mounted and tested on one of his own monoplanes (the Fokker A.III). German pilots Oswald Boelcke and Max Immelmann both received the first prototypes, which were designated the Fokker E.I (dubbed the “Eindecker”), in early summer 1915. Although their 80 hp Oberursel UO rotary motor proved to be underpowered, both Boelcke and Immelmann succeeded in shooting down enemy aircraft. Convinced of its success, German authorities adopted it and Fokker rushed it into production.

Although only a few E.1 versions were built, 23 Fokker E.II fighters entered service in September 1915, before the most common variety, the E.III, of which approximately 150 were constructed, began to enter service in late 1915. Whereas the E.II and E.III were both powered by a 100 hp Oberursel U.I 9-cylinder rotary engine, the E.III featured some design modifications to strengthen its wings and improve its maneuverability. The E.III had a wingspan of 31 ft 2.75 in., a length of 23 ft 7.5 in., and a loaded weight of 1,342 lb. Its 100 hp Oberursel rotary motor could produce a maximum speed of 81 mph, could climb 1,000 m (3,281 ft) in 5 minutes, and had a service ceiling of approximately 3,500 m (11,482 ft). The Eindecker was a solid aircraft that featured the use of welded steel tubing for the fuselage frame. The wings, which were mounted to the side of the fuselage with two I-section main spars, were braced by cables that were attached to the undercarriage and a central pylon in front of the pilot’s seat. An additional set of cables ran through pulleys and were attached to the control stick and wings to allow the pilot to warp the wings for lateral control. At first the Germans intended to use the Eindecker to provide protection for their own reconnaissance aircraft; consequently, they spread them out by placing two with each squadron. As Boelcke and Immelmann began to range out on their own and shoot down enemy aircraft, however, the Germans gradually began to concentrate them for greater effect during the winter of 1915–1916, a period that the Allies came to call the “Fokker Scourge.” Even though the Eindecker owed much of its success to its synchronization gear, it must be noted that Allied aircraft at the time, particularly the R.A.F. B.E.2, which placed the armed observer in the front seat, were helpless when attacked from the rear. Nevertheless, it must be emphasized that Boelcke and Immelmann would use their Eindeckers to develop the basic fighting tactics and maneuvers that would remain standard throughout the war. By late spring 1916, new British and French biplanes, which were faster and more maneuverable, were eclipsing the Eindecker. Fokker attempted to extend their life by introducing the E.IV, which was slightly larger and powered by a two-row 160 hp Oberursel U III rotary engine. The increased weight and torque made it unsuccessful and only about 30 were produced.

Variants

The Eindecker went through five variants:

  1. Fokker M.5K/MG (A.III) - 5 built
  2. Fokker E.I - 68 built
  3. Fokker E.II - 49 built
  4. Fokker E.III - 249 built
  5. Fokker E.IV - 49 built

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Stuka Photoalbum

Posted on December 01 2009 at 06:52 PM

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