RD-0109

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RD-0109

Part of S1

RD-0109
Credit: KBKhA

Kosberg LOx/Kerosene rocket engine. 8A92 Vostok stage 3, 8K72K stage 3 (block E-Vostok). Out of production. Developed in 15 months. First flight 1960.

AKA: 8D719;RD-448;RD-448, RO-7;RO-7. Status: Out of production. Date: 1959-60. Number: 154 . Thrust: 54.52 kN (12,257 lbf). Unfuelled mass: 121 kg (266 lb). Specific impulse: 324 s. Burn time: 430 s. Height: 1.58 m (5.18 ft). Diameter: 0.76 m (2.49 ft).

Engine: 121 kg (266 lb). Chamber Pressure: 50.00 bar. Area Ratio: 79.4. Propellant Formulation: Lox/RG-1. Thrust to Weight Ratio: 45.95.

Country: Russia. Launch Vehicles: Vostok 8K72K, Vostok 8A92, Vostok 8A92M. Propellants: Lox/Kerosene. Stages: Vostok 8K72K-2, Vostok 8A92-2, Vostok 8A92M-2. Agency: Kosberg bureau. Bibliography: 307, 320, 95, 7466.

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