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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 ...
The related Type 65 variant was instead based on the T-34-85 chassis. None of the original Type 63's survive today. [3] The Type 65 retained the hull from the T-34-85 but the turret was replaced by an open-top box turret armed with twin Type 61 37mm anti-aircraft guns. [1] [2] The guns were loaded manually with 5-round clips.
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 ...
Designed at the Kharkiv Locomotive Factory by Konstantin Chelpan and his team, it is found in the BT-7M (BT-8), T-34, KV, IS and IS-10 (T-10) tanks, and by extension, the vehicles based on them, such as the SU-85 and SU-100 tank destroyers based on the T-34 and the ISU-122 and ISU-152 self-propelled guns based on the IS-2. Throughout its ...
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 ...
The major changes made to both Heavy Tanks T34 were linked to gunnery trials. Due to the bulky ammunition, the ammunition capacity was the same as the Heavy Tank T30 34 rounds. On the other hand, the lighter ammunition made loading the gun faster, especially with two loaders. The maximum rate of fire was 5 RPM, impressive for such a caliber.