Status: Out of Production. First Launch: 1950s late. Thrust: 167.00 kN (37,543 lbf). Unfuelled mass: 122 kg (268 lb). Height: 1.02 m (3.33 ft). Diameter: 0.62 m (2.05 ft).
Throttled thrust(vac): 49.000 kN (11,015 lbf). Engine: 122 kg (268 lb). Propellant Formulation: AK27I/TG-02. Thrust to Weight Ratio: 139.34.