Status: Developed 1941-46. Date: 1941-46. Thrust: 2.94 kN (661 lbf). Unfuelled mass: 60 kg (132 lb). Specific impulse: 200 s.
Engine: 60 kg (132 lb). Chamber Pressure: 22.00 bar. Thrust to Weight Ratio: 5.
Family: Storable liquid. Country: Russia. Propellants: Nitric acid/Kerosene. Agency: Glushko bureau. Bibliography: 342. 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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