|Role||Heavy bomber/Civilian transport|
|National origin||Soviet Union|
|Status||Destroyed in crash|
The Kalinin K-7 (Russian: Калинин К-7; Ukrainian: Калінін К-7) was a heavy experimental aircraft designed and tested in the Soviet Union in the early 1930s. It was of unusual configuration, with twin booms and large underwing pods housing fixed landing gear and machine gun turrets. In the passenger version, seats were arranged inside the 2.3-meter thick (7 ft 7 in) wings. The airframe was welded from KhMA chrome-molybdenum steel. The original design called for six engines in the wing leading edge, but when the projected loaded weight was exceeded, two more engines were added to the trailing edges of the wing, one right and one left of the central passenger pod. Nemecek states in his book that at first only one further pusher engine was added.
Design and development
Designed by World War I and Civil War pilot Konstantin Kalinin at the aviation design bureau he headed in Kharkiv, with a wingspan close to that of a Boeing B-52 Stratofortress and a much greater wing area, the K-7 was one of the biggest aircraft built before the jet age. It had an unusual arrangement of six tractor engines on the wing leading edge and a single engine in pusher configuration at the rear.
In civil transport configuration, it would have had a capacity for 120 passengers and 7,000 kg (15,000 lb) of mail. As a troop transport it would have had capacity for 112 fully equipped paratroopers. In bomber configuration it would have been armed with 8 x 20mm autocannons, 8 x 7.62mm machine guns and up to 9,600 kg (21,200 lb) of bombs.
The K-7 first flew on 11 August 1933. The very brief first flight showed instability and serious vibration caused by the airframe resonating with the engine frequency. The solution to this was thought to be to shorten and strengthen the tail booms, little being known then about the natural frequencies of structures and their response to vibration. The aircraft completed seven test flights before a crash due to structural failure of one of the tail booms on 21 November 1933.
The existence of the aircraft had only recently been announced by Pravda, which declared it was "victory of the utmost political importance," since it had been built with USSR steel, rather than imported steel. The accident killed 14 people aboard and one on the ground. Flight speculated that sabotage was suspected as the investigating committee had representation by the state security organization, the Joint State Political Directorate (OGPU).
However, there appeared recently some speculation in the Russian aviation press about the role of politics and the competing design office of Andrei Tupolev, suggesting possible sabotage. Although two more prototypes were ordered in 1933, the project was cancelled in 1935 before they could be completed.
Data from Shavrov (1985)
- Crew: minimum 11
- Capacity: 120 passengers in civilian configuration
- Length: 28 m (91 ft 10 in)
- Wingspan: 53 m (173 ft 11 in)
- Height: 12.4m (estimated to top of engine shell)
- Wing area: 454 m² (4,886.8 ft²)
- Empty weight: 24,400 kg (53,793 lb)
- Loaded weight: 38,000 kg (83,776 lb)
- Powerplant: 7 × Mikulin AM-34F V-12 piston engines, 560 kW (750 hp) each
- Maximum speed: 225 km/h (121 knots, 140 mph)
- Service ceiling: 4,000 m (13,123 ft)
- Wing loading: 84 kg/m² (17 lb/ft²)
- Power/mass: 103 W/kg (0.06 hp/lb)
- Shavrov (1985)[page needed]
- Nemecek (1986)
- Bill Gunston (1991). Giants of the sky: the biggest aeroplanes of all time. Patrick Stephens. p. 119. ISBN 1852602589.
- Bill Yenne. The World's Worst Aircraft.
- "The K-7 disaster Flight, November 30, 1933 p1201
- "Huge Soviet Plane Crashes, Killing 14". New York Times. November 23, 1933.
- Gunston, Bill (1995). The Osprey Encyclopedia of Russian Aircraft 1875–1995. London: Osprey Publishing. ISBN 1-85532-405-9.
- Nemecek, Vaclav (1986). The History of Soviet Aircraft from 1918. Willow Books. ISBN 978-0002180337.
- Shavrov, V. B. (1985). Istoriya konstruktskii samoletov v SSSR do 1938 g. (3 izd.) (in Russian). Mashinostroenie. ISBN 5-217-03112-3.
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