Status: Out of Production. Date: 1957. Thrust: 34.60 kN (7,778 lbf). Specific impulse: 277 s.
Throttled thrust(vac): 13.700 kN (3,080 lbf). Chamber Pressure: 37.30 bar. Propellant Formulation: LOX/TS1.
Country: Russia. Propellants: Lox/Kerosene. Agency: Kosberg bureau. Bibliography: 309. Back to top of page Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9RetroSearch is an open source project built by @garambo | Open a GitHub Issue
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