RD-0109
Engine · Russia
Original archive entry. The text, images and links below are kept as they were written.
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.
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.
Related
- Country
- Russia
- Launch Vehicles
- Vostok 8K72K, Vostok 8A92, Vostok 8A92M
- Propellants
- Lox/Kerosene
- Agency
- Kosberg bureau