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
RD-254
Part of RD-253
Glushko N2O4/UDMH rocket engine. N-1 upper stage, UR-700 stage 3. Proposed for use in N-1. High altitude version of RD-253 for 2nd stages. Later proposed for R-56 and UR-700 upper stages.

Status: Study 1961. Date: 1962-66. Thrust: 1,716.00 kN (385,772 lbf).

Family: Storable liquid. Country: Russia. Propellants: N2O4/UDMH. Stages: R-56 Block B, UR-700-3. Agency: Glushko bureau. Bibliography: 323.
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