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https://en.wikipedia.org/wiki/Westland_Lysander
The Westland Lysander was a British army co-operation and liaison aircraft produced by Westland Aircraft used immediately before and during the Second World War. After becoming obsolete in the army co-operation role, the aircraft's exceptional short-field performance enabled clandestine missions using small, unprepared airstrips behind enemy lines to place or recover agents, particularly in occupied France with the help of the French Resistance. British army air co-operation aircraft were named after mythical or historical military leaders; in this case the Spartan general Lysander was chosen. Despite its appearance, the Lysander was aerodynamically advanced; it was equipped with fully automatic wing slots and slotted flaps and a variable incidence tailplane. These refinements gave the Lysander a stalling speed of only 65 mph (104 km/h, 56.5 knots). It also featured the largest Elektron alloy extrusion made at the time: a single piece inside the spats supporting the wheels. This was a feature of British-built aircraft only – Canadian-built machines had a conventionally fabricated assembly due to the difficulties involved in manufacturing such a large extrusion. The Air Ministry requested two prototypes of the P.8 and the competing Bristol Type 148, quickly selecting the Westland aircraft for production and issuing a contract in September 1936. Role Army co-operation and liaison aircraft Manufacturer Westland Aircraft Designer Arthur Davenport, Teddy Petter First flight 15 June 1936 Introduction June 1938 Retired 1946 (UK) Primary users Royal Air Force Indian Air Force Royal Canadian Air Force Egyptian Air Force United States Army Air Forces Number built 1,786 The first Lysanders entered service in June 1938, equipping squadrons for army co-operation and were initially used for message-dropping and artillery spotting. When war broke out in Europe, the earlier Mk Is had been largely replaced by Mk IIs, the older machines heading for the Middle East. Some of these aircraft, now designated type L.1, operated with the Chindits of the British Indian Army in the Burma Campaign of the Second World War. Lysanders flew dawn and dusk patrols off the coast and in the event of an invasion of Britain, they were tasked with attacking the landing beaches with light bombs and machine guns. They were replaced in the home-based army co-operation role from 1941 by camera-equipped fighters such as the Curtiss Tomahawk and North American Mustang carrying out reconnaissance operations, while light aircraft such as the Taylorcraft Auster were used to direct artillery. Some UK-based Lysanders went to work operating air-sea rescue, dropping dinghies to downed RAF aircrew in the English Channel. Fourteen squadrons and flights were formed for this role in 1940 and 1941. Lysanders flew from secret airfields at Newmarket and later Tempsford, but used regular RAF stations to fuel-up for the actual crossing, particularly RAF Tangmere. Flying without any navigation equipment other than a map and compass, Lysanders would land on short strips of land, such as fields, marked out by four or five torches. Or to avoid having to land, the agent, wearing a special padded suit, stepped off at very low altitude and rolled to a stop on the field. They were originally designed to carry one passenger in the rear cockpit, but for SOE use the rear cockpit was modified to carry two passengers in extreme discomfort in case of urgent necessity. The pilots of No. 138 and from early 1942, No. 161 Squadron transported 101 agents to and recovered 128 agents from Nazi-occupied Europe. The Germans knew little about the British aircraft and wished to study one. Soldiers captured an intact Lysander in March 1942 when its pilot was unable to destroy it after a crash, but a train hit the truck carrying the Lysander, destroying the cargo. Specifications (Lysander Mk III) General characteristics Crew: One, pilot Capacity: 1 passenger (or observer) Length: 30 ft 6 in (9.29 m) Wingspan: 50 ft 0 in (15.24 m) Height: 14 ft 6 in (4.42 m) Wing area: 260 ft² (24.2 m²) Empty weight: 4,365 lb (1,984 kg) Max. takeoff weight: 6,330 lb (2,877 kg) Powerplant: 1 × Bristol Mercury XX radial engine, 870 hp (649 kW) Performance Maximum speed: 212 mph (184 knots, 341 km/h) at 5,000 ft (1,520 m) Range: 600 miles (522 nmi, 966 km) Service ceiling: 21,500 ft (6,550 m) Climb to 10,000 ft (3,050 m): 8 min Take-off run to 50 ft (15 m): 305 yards (279 m) Armament Guns: Two forward-firing .303 in (7.7 mm) Browning machine guns in wheel fairings and two more for the observer Bombs: Four 20 lb (9 kg) bombs under rear fuselage and 500 lb (227 kg) of bombs on stub wings if fitted The Lysander’s failure to protect itself from the enemy in the Spring of 1940 led to the development of a prototype called the Delanne Tandem Wing or Lysander P12. Westland designers worked with Frenchman Maurice Henri Delanne to develop more lift at the back of the aircraft to allow for a heavy defensive machine gun turret at the rear. Only one prototype was constructed—from test bed K6127. The large yellow P in a circle roundel on K6127 denoted a prototype. * |
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