Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z
RO-31
Part of RD-0411
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.

Status: Study 1967. Thrust: 392.00 kN (88,125 lbf).

Propellant Formulation: Nuclear/LH2/Methane.

Family: nuclear-powered. Country: Russia. Launch Vehicles: UR-700 / RO-31. Propellants: Nuclear/LH2. Stages: UR-700-RO-31. Agency: Kosberg bureau. Bibliography: 443.
Back to top of page
Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z
© 1997-2019 Mark Wade - Contact
© / Conditions for Use