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Thursday, February 12, 2009

Samolot mysliwsko-bombowy Su-22

Samolot mysliwsko-bombowy Su-22 Military Papercraft


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Like the Buccaneer, the SU22 was designed as a high speed, medium range, low level ground attack / recce aircraft. The main design difference between the two being that the SU22 was never intended for carrier operations and from the outset had a limited air-to-air capability. Although its origin can be traced back to the basic SU7 aircraft of the 1950’s, the design was continuously developed emerging as the variable geometry (Swing-wing 30:63) SU17 / 22, the most modern and powerful Warsaw Pact fighter bomber. The NATO code name for the type was “Fitter”.

The design exemplifies two key traits synonymous with Russian military equipment; the twin virtues of Simplicity & Robustness, both in the physical construction of the aircraft as well as its operation. The intent was to have trouble free use under the most demanding operating and environmental conditions combined with ease of maintenance. Both the airframe and the Lyulka AL-21 F-3 engine more than met this challenge!


The SU22M-4 is the final export version of the type and represents the pinnacle in the evolution of the design. It is still widely used in Europe and the Middle East, being broadly compatible to a Tornado GR1 although lacking the latter’s all-weather capability. Like the Tornado it is equipped with a laser range finder designator and terrain following radar and could be equipped with bombs, guided missiles & rockets in addition to the installed twin 30mm canon for the air to surface attack role. Air-to-air threats were countered via rockets, guided missiles and canon in addition to the extensive ECM and chaff / flare systems.

HHA operate one SU22M4, its supersonic capability and ten hardpoints enabling a variety of threat simulation profiles to be flown. Our aircraft is the only one of its type being operated by a civilian company and was acquired from the German Air Force.

Initially delivered on the 26-11-1986 as “629” of the NVA (East German Air Force), it served with 2/ MFG 28 (2nd Squadron, Naval wing 28) at Laage until it was prematurely retired on the 2-10-90 as a result of the collapse of the East German regime.

The German MoD had decided not to keep the SU22 on its inventory, and as a result the East German Squadrons were disbanded and the aircraft was placed in airworthy store under the new squadron code “25+29”. However, the aircraft was still very much a potent strike aircraft in use all over the world, so the German Test and Evaluation Centre (WTD –61) at Manching acquired seven of the type for technological evaluation purposes. Our SU was one of these and became “98+14” with its new owners on 23-9-1991. The aircraft were test flown and maintained by former NVA personnel, with major servicing being undertaken by the Polish aircraft facility WZL-2 at Bydgoszcz. West German pilots and ground crews were rapidly brought up to speed on the type and the evaluation of its systems lasted until September 1998.


After extensive negotiations HHA acquired the aircraft on the 14 January 1999 when it was flown to our maintenance facility at RAF Scampton. When delivered, the aircraft had accrued only 767 flight hours in 743 flights and became the youngest & lowest houred aircraft in our fleet.






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Radziecki czotg tywajacy T-38 M2

Radziecki czotg tywajacy T-38 M2 Military Papercraft



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M2 Light Tank


Type Light tank
Place of origin United States
Specifications
Weight 11.6 tonnes (25,600 lb)
Length 4.43 m (14.53 ft)
Width 2.47 m (8.1 ft)
Height 2.65 m (8.69 ft)
Crew 4 (Commander/gunner, loader, driver, co-driver)
Armor 6 - 25 mm (0.25 - 1.0 in)
Primary
armament 1x 37 mm Gun M5
103 rounds
Secondary
armament 5x .30-06 Browning M1919A4 machine guns
8,470 rounds
Engine Continental W-670-9A, 7 Cylinder
245/220 hp (183/164 kW)
Power/weight hp/tonne
Suspension Vertical Volute Spring Suspension (VVSS)
Operational
range 320 km (199 mi)
Speed 58 km/h (36 mi/h)

The Light Tank M2 was an American pre-World War II light tank that saw use in early battles of the Pacific War. Although only a few saw combat, it was an important development step in the line of US light tanks of World War II.

Development History

As the Light Tank T2E1, the M2 was developed in 1935 by Rock Island Arsenal for the infantry branch of the U.S. Army. The design coming from the earlier T1 and T2 was somewhat inspired by the famous Vickers 6-ton. Its main weapon was one .50 machine gun, installed in a small one-man turret. After only 10 units were delivered, the Infantry branch decided to switch to a twin turret configuration, with a .30 machine gun in the second turret. These early twin-turret tanks were given the nickname "Mae West" by the troops, after the popular movie star. The twin-turret layout was inefficient, but was a common feature of 1930s light tanks derived from the Vickers, such as the Soviet T-26 and Polish 7TP.

Following the Spanish Civil War, the U.S. Army understood it needed better arms and better armored vehicles. The Cavalry branch had already opted for a single, larger turret on its nearly identical M1 Combat Car. By 1940 the twin machine gun turrets were replaced by one larger turret with a 37 mm gun, and armor reached 25 mm. Other upgrades included improved suspension, improved transmission, and better engine cooling.

The Battle of France gave momentum to the US tank program, and in July 1940 work began on a new light tank based on the M2 series. By adding heavier armor and a slightly longer hull, the M3 was created. The early M3 closely resembled the M2A4 and indeed the two types occasionally served in the same units; the easiest recognition feature is the idler wheel. On the M2A4, the idler is raised; on the M3 it trails on the ground, increasing the flotation of the heavier vehicle. In March 1941 light tank production switched to the M3 series.

The M2's importance lies in the sound basis it provided for US M3-series light tanks early in WW2. The M3's high speed and mechanical reliability were legacies of the M2 program.[citation needed]


Employment

By December 1941, the M2A1, M2A2 and M2A3 were used for training only. A few M2A4 saw some combat in the Battle of Guadalcanal with the U.S. Marine Corps and remained in service in some areas of Pacific until 1943.

Britain ordered 100 M2A4s in early 1941. After 36 of them were delivered, the order was canceled in favor of an improved Light Tank M3.

M2A2 "Mae West" on display at Patton Cavalry and Armor Museum, Fort Knox, KY
  • M2A1 (1935).
    • .50 MG in a single turret. 10 units were produced.
  • M2A2 (1935).
    • Twin turrets. Dubbed "Mae West". 239 units produced.
  • M2A3 (1938).
    • Twin turrets, Thicker armor, improved suspension. 72 units produced.
  • M2A4 (1940).
    • Single turret with 37mm gun. Thicker armor. 375 units produced.


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Tuesday, February 10, 2009

SAMOLOT TOWARZYSZACY LUBLIN R-XIII D

SAMOLOT TOWARZYSZACY LUBLIN R-XIII D


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The Lublin R-XIII was the Polish army-cooperation plane (observation and liaison plane), designed in the early-1930s in the Plage i Laśkiewicz factory in Lublin. It was the main army cooperation plane in the Invasion of Poland. Its variant Lublin R-XIV was a military trainer aircraft.



Design and development

In 1927, the Polish aviation authorities announced a contest for an army-cooperation plane (in Polish: samolot towarzyszący, literally: acompanying plane. In Polish doctrine it was a close reconnaissance, observation and liaison aircraft, operating from casual airfields, providing big Army land units with information about the enemy). The PZL state factory proposed the PZL Ł-2, built in a series of 25 aircraft, while private factory Plage i Laśkiewicz in Lublin proposed the Lublin R-X, designed by Jerzy Rudlicki. It was flown on February 1, 1929. Five aircraft were built for the Air Force as R-Xa, and one was built as a long-distance sports plane. The third competitor was the PWS-5t2.

The contest was won by the R-Xa, having the shortest take-off and landing, and good performance, but the factory was ordered to develop design further. At that time, Rudlicki was working upon an unarmed trainer aircraft R-XIV and an observation aircraft R-XV. Both were new designs, basing upon the R-X construction (a trivia is, that number XIII was initially omitted in designations as "unlucky"). In February 1930, the Polish Air Force ordered 15 of R-XIV. The first serial plane was built in June 1930, without an earlier prototype, and all were delivered by July 1931. The R-XIV was a two-seater, parasol wing aircraft, with a 220hp radial engine and fixed landing gear. The crewman sat in open cabs in tandem. The R-XV was not ordered, but the Air Force demanded instead, that two R-XIV should be armed with an observer's machine gun, for testing. Such armed R-XIV, fitted also with other minor modifications, most notably a changed shape of a tail fin, became the first prototype of the army-cooperation plane, that received a designation Lublin R-XIII.

In July 21, 1931, 50 aircraft R-XIII were ordered. The first series of 30 were designated R-XIIIA, the next 20 were R-XIIIB. Both variants differed mostly in a type of a machine gun ring mounting. The first serial R-XIII was built on June 7, 1932. By March 11, 1933, all were given to the Air Force.

In 1932, next 170 aircraft were ordered. 48 were built in R-XIIIC variant with minor modifications, then 95 were built in a most numerous R-XIIID variant. It introduced visible changes, like a Townend ring on a radial engine, and a new engine cowling. It also had new type of a machine gun ring mounting. The first R-XIIID was tested in February, 1933. All aircraft were given to the Air Force by March 2, 1935. During repairs, older models A, B and C were modified to R-XIIID standard as well.

In 1933, Jerzy Rudlicki proposed a new design R-XXI, for a new contest for R-XIII successor, but it was not accepted (the contest was won by the RWD-14 Czapla). However, some of R-XXI features, like higher and rounded in cross-section fuselage and changed shape of a tail fin, were found in latest R-XIII variants. Single prototype of the R-XIIIE was built in 1934, fitted with a stronger 360hp engine Gnome-Rhone 7K Titan, but it was not produced. Another variant R-XIIIF introduced new, Polish-designed 340hp engine Skoda G-1620A Mors-I. It had no Townend ring on cylinders of the radial engine. After one prototype (no. 56.101), a series of 50 R-XIIIF were ordered in 1934. After 7 aircraft had been delivered, the Polish aviation authorities refused to buy nearly-completed further 18 aircraft, planning to nationalize all aviation industry in Poland. As a result, Plage i Laśkiewicz factory went bankrupt in late 1935, and it was next nationalized under a name LWS (Lubelska Wytwórnia Samolotów - Lublin Aircraft Works). Then, 18 R-XIIIF, bought by scrap price, were completed, and next series of 32 was built. All R-XIIIF were delivered to the Air Force by 1938. However, only 26 of them were completed with Mors engines (and mostly used for training or staff liaison), while 32 had standard 220hp Wright engines, lowering their performance to R-XIIID level.

In 1931, one R-XIV was tested on floats, as a seaplane. Since tests came out well, the Polish Navy designated it R-XIII bis/hydro and ordered the next three (nos. 700-703). In 1933, the Navy ordered 10 R-XIII ter/hydro, which was a seaplane variant of R-XIIID (nos. 704-713). Finally, in 1934 the Navy bought 6 R-XIIIG seaplanes, differing in details from a previous variant - among others, a metal propeller (nos. 714-720). They were delivered by April 1935. All variants could also be easily converted to wheeled landing gear.

In 1933, one R-XIIIB was converted to a long-distance sport plane R-XIIIDr, named Błękitny Ptak (the Blue Bird), meant for a flight to Australia, however it was crashed in 1935 in Siam by Stanisław Karpiński. Several aircraft were converted to civilian sport ones, used in aeroclubs.

12 R-XIII's were converted to blind flying trainers R-XIIIt in 1934, with higher closed trainee cab. Some were converted to simple liaison aircraft, removig armament and mounting a windscreen in the second cab. Several R-XIII were used to tow gliders, using a special frame with a hook, attached to a fuselage.

The R-XIII prototype was converted in 1932 to an experimental variant R-XIX, with V-tail of Rudlicki's design, but it was not accepted by the authorities, despite it had better field of machine gun fire.

In total, 15 R-XIV and 273 R-XIII were built, including 20 seaplanes.

Combat use

In the early 1930s the R-XIII was quite a successful plane for its purpose. It had a very short take-off (68 m for R-XIIIA) and landing, enabling it to operate from fields and meadows. However, only some of R-XIIIs were equipped with a radio and a camera, what lowered their usefulness. In 1932-1936 they were used in three-aircraft liaison platoons, being a basic Polish army-cooperation plane. In 1937 they were formed into army-cooperation escadres (eskadra towarzysząca), in 1939 reformed into observation escadres (eskadra obserwacyjna). Only in 1939, part of R-XIII were replaced by the RWD-14b Czapla, which was not much more modern. A planned replacement was a modern LWS-3 Mewa, but it was not introduced due to war outbreak.

In the Invasion of Poland in 1939, the Polish Air Force had about 150 R-XIII. Of them, 49 were in combat units, 30 in reserve, about 30 in training units and about 40 in repairs. In combat units, R-XIII were used in 7 observation escadres (out of 12): numbers 16, 26, 36, 43, 46, 56 and 66. Each escadre had 7 aircraft. The 16th Escadre was in C-in-C reserve, while the others were distributed among the field Armies. The R-XIII was no match for any of Luftwaffe fighters, bombers or even reconnaissance aircraft, being much slower, and armed with only one machine gun, but they were actively used for close reconnaissance and liaison tasks.

About 40 R-XIII of combat units were destroyed during the campaign, but only part of them were shot down by the German aircraft or flak. During the campaign, 9 aircraft were given to observation escadres as replenishment. Some planes were also used in a wartime improvised units in air bases. About 10 combat aircraft and 7 from other units were withdrawn to Romania. A number of aircraft were bombed by the Germans in air bases or burned by withdrawing Poles. None have survived to today.

In the Naval Air Squadron, 11 R-XIIIter and R-XIIIG floatplanes were used in 1939. One of them made a night bombing raid on Danzig on September 7, searching in vain for Schleswig-Holstein. On September 8 all planes were bombed, while stationed on the sea near Hel on Hel Peninsula.

Variants

  • R-XIII prototype (conversion of R-XIV, no. 56.1)
  • R-XIIIA - army cooperation aircraft, 30 produced from 1931 (nos 56.2-56.31)
  • R-XIIIB - army cooperation aircraft, 20 produced from 1932 (nos 56.32-56.51)
  • R-XIIIC - army cooperation aircraft, 48 produced from 1933 (nos. 56.52-56.99)
  • R-XIIID - standard variant of army cooperation aircraft, 95 produced from 1933 (nos 56.102-56.196)
  • R-XIIIE - one prototype of 1934 with 360hp Gnome-Rhone 7K Titan engine (no. 56.100)
  • R-XIIIF - army cooperation aircraft with modified fuselage, part with 340hp Skoda G-1620A Mors-I engine, 58 produced from 1934 (nos. 56.101, 58.01-58.57)
  • R-XIII bis/hydro - seaplane, 4 produced from 1931 (nos. 700-703)
  • R-XIII ter/hydro - seaplane, 10 produced from 1934 (nos. 704-713)
  • R-XIIIG - seaplane, 6 produced from 1934 (nos. 714-720)
  • R-XIIIDr - long-distance sport conversion, 1 made (no. 56.51)
  • R-XIIIt - trainer conversion, at least 12 made
  • R-XIV - trainer, 15 produced from 1930 (nos. 54.1-54.15)
  • R-XV - army cooperation variant of R-XIV, not built
  • R-XIX - one prototype with V-tail of 1932 (no. 56.1)
  • R-XXIII - This was the original designation of the R-XIIIDr.

Description

Mixed construction (steel and wood) plane, conventional in layout, with braced high-wings, canvas and plywood covered (front part of a fuselage was metal covered). Conventional fixed landing gear, with a rear skid. Crew of two, sitting in tandem in an open cockpit, with twin controls. The observer had a 7.7 mm Vickers K or Lewis machine gun on a ring mounting (rarely 2 machine guns). The aircraft could be fitted with racks for small bombs 12–25 kg. A 9 cylinder air-cooled radial engine Wright Whirlwind J-5 (produced in Poland) with 162 kW (220 hp) nominal power and 176 kW (240 hp) take-off power (on 22 aircraft R-XIIIF, 250 kW (340 hp) engine Skoda G-1620A Mors-I). Two-blade wooden or metal propeller. Fuel tank 200 liters in the fuselage, could be dropped in case of fire emergency (R-XIV - 135 liter tank).

Operators

Specifications (R-XIIID)

General characteristics

  • Crew: 2 - Pilot and observer
  • Length: 8.5m ()
  • Wingspan: 13.2m ()
  • Height: 2.8m ()
  • Wing area: 24.50m2 ()
  • Empty weight: 956kg (2,108lb)
  • Loaded weight: 1332kg (2,930lb)
  • Powerplant:Wright Whirlwind J-5 9-cylinder radial engine, 162kW (220hp)

Performance



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