Status: Out of Production. Thrust: 200 N (40 lbf). Unfuelled mass: 5.50 kg (12.10 lb). Specific impulse: 265 s.
Engine: 5.50 kg (12.10 lb). Thrust to Weight Ratio: 3.63.
Country: Russia. Propellants: GOX/Kerosene. Agency: NII Mash. Bibliography: 336. 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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