S5.44
Engine · Russia
Original archive entry. The text, images and links below are kept as they were written.
Isayev Nitric acid/Amine rocket engine. SAM-missile 5Ya24. Out of Production. Could be throttled. 177-49 kN sea-level. Area ratio 118 - 44.
Throttled thrust(vac): 49.000 kN (11,015 lbf). Engine: 124 kg (273 lb). Area Ratio: 118. Propellant Formulation: AK27I/TG-02. Thrust to Weight Ratio: 145.16.
Related
- Family
- Storable liquid
- Country
- Russia
- Launch Vehicles
- S-25
- Propellants
- Nitric acid/Amine
- Agency
- Isayev bureau