RD-0201
Engine · Russia
Original archive entry. The text, images and links below are kept as they were written.
Kosberg Nitric acid/Amine rocket engine. SAM V1100 by Grushin stage 3. Out of Production. Thrust range 59 - 28 kN. First flight 1960.
Chambers: 4. Throttled thrust(vac): 28.000 kN (6,294 lbf). Engine: 120 kg (260 lb). Chamber Pressure: 62.00 bar. Propellant Formulation: AK27P/TG-02. Thrust to Weight Ratio: 49.33.
Related
- Family
- Storable liquid
- Country
- Russia
- Propellants
- Nitric acid/Amine
- Agency
- Kosberg bureau