Status: Design concept 1965-94. Date: 1965-94. Thrust: 392.00 kN (88,125 lbf). Specific impulse: 900 s.
Subtopics RO-31 Kosberg nuclear/LH2 rocket engine. UR-700 Third Stage. Study 1967. Engine proposed for UR-700 third stage to achieve 250 metric ton payload to low earth orbit. Probably closely related to RD-0411. Family: nuclear-powered. Country: Russia. Propellants: Nuclear/LH2. Agency: Kosberg bureau. Bibliography: 307, 95. 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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