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RD-0105


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RD-0105
Credit: KBKhA Kosberg LOx/Kerosene rocket engine. Luna 8K72, Vostok 8K72 upper stage. Out of production. Developed jointly with OKB-1 in nine months on the basis of OKB-1's steering chamber from the RD-107 engine. First flight 1958.

AKA: 8D714;RD-428;RO-5;RO-5, RD-428. Status: Out of production. Date: 1957-59. Number: 13 . Thrust: 49.40 kN (11,106 lbf). Unfuelled mass: 125 kg (275 lb). Specific impulse: 316 s. Burn time: 440 s. Diameter: 2.56 m (8.39 ft).

Engine: 125 kg (275 lb). Chamber Pressure: 45.00 bar. Thrust to Weight Ratio: 40.

Country: Russia. Launch Vehicles: Vostok 8K72, Vostok-L 8K72. Propellants: Lox/Kerosene. Stages: Luna 8K72-2, Vostok 8K72-2. Agency: Kosberg bureau. Bibliography: 174, 307, 344, 7463. Back to top of page Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
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