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-0235
Part of RD-0216 Family
RD-0235
RD-0235
Credit: KBKhA
Kosberg N2O4/UDMH rocket engine. UR-100N / RS-18 (SS-19) stage 2. Main engine based on RD-0217 with larger nozzle for altitude operation. Staged combustion cycle. First flight 1972.

Date: 1969-74. Number: 315 . Thrust: 240.00 kN (53,950 lbf). Specific impulse: 320 s.

Chamber Pressure: 175.00 bar.



Family: Storable liquid. Country: Russia. Launch Vehicles: UR-100N, Rokot. Propellants: N2O4/UDMH. Stages: UR-100N Stage 2N. Agency: Kosberg bureau. Bibliography: 339, 353, 7488.

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
© 1997-2017 Mark Wade - Contact
© / Conditions for Use