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Interior of a T-34-85 viewed from the driver's hatch, showing the ammunition boxes on which the loader had to stand in the absence of a turret basket. In the foreground is the driver's seat. Levers for radiator flaps can be seen on the firewall. Production of the T-34-85 began in January 1944 at Factory No. 112, first using the D-5T 85 mm gun.
The Beechcraft T-34 Mentor is an American propeller-driven, single-engined, military trainer aircraft derived from the Beechcraft Model 35 Bonanza. The earlier versions of the T-34, dating from around the late 1940s to the 1950s, were piston-engined. These were eventually succeeded by the upgraded T-34C Turbo-Mentor, powered by a turboprop ...
OT-34-85 (sometimes called TO-34) - A T-34-85 flamethrower tank, fitted with a ATO-42 in place of the bow machine gun. T-34-100 - OKB #9 Factory #183 built one example armed with a 100mm ZIS-100. Attempts were also made to mount a 100mm D-10-34 in a T-34-85 turret and a prototype T-44 turret. Due to the added weight of the new gun, the bow ...
Twin piston engine monoplane utility airplane Beechcraft Model 87: 1 Prototype twin turboprop engine monoplane utility airplane [2] Beechcraft Model 88 Queen Air: 1965 47 Twin piston engine monoplane utility airplane Beechcraft Model 89 Queen Airliner: N/A 0 Unbuilt twin piston engine monoplane utility airplane Beechcraft Model 90 King Air ...
The M26 and M46 proved to be an overmatch for the T-34-85 as their 90 mm HVAP round could punch all the way through the T-34 from the front glacis armour to the back, whereas the T-34-85 had difficulty penetrating the armour of the M26 or the M46. The M4A3E8, firing 76 mm HVAP rounds, was a closer match to the T-34-85 as both tanks could ...
Developed from the T65 40 mm GMC (anti-aircraft gun on extended M5 chassis). Lengthened M24 hull with engine moved to center, twin 40 mm Bofors anti-aircraft guns mounted at hull rear (336 rounds). 904 were ordered in August 1944, but only 285 were completed by the end of the war. [18] M37 105 mm howitzer motor carriage; Developed in 1945.
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Data from Jane's All The World's Aircraft 1966–1967 General characteristics Crew: 2 Length: 7.94 m (26 ft 1 in) Wingspan: 10.0 m (32 ft 10 in) Height: 2.92 m (9 ft 7 in) Wing area: 16.49 m 2 (177.5 sq ft) Empty weight: 1,134 kg (2,500 lb) Max takeoff weight: 1,750 kg (3,858 lb) Fuel capacity: 189 L (50 US gal; 42 imp gal) normal, provision for further 76 L (20 US gal; 17 imp gal) in ...