Status: Design concept 1998-. Date: 1998-. Thrust: 343.00 kN (77,109 lbf). Specific impulse: 370 s.
Country: Russia. Propellants: Lox/LNG. Agency: Kosberg bureau. Bibliography: 328. 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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