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-0234
Kosberg N2O4/UDMH rocket engine. UR-100N / RS-18 (SS-19) stage 1. Out of Production. Staged combustion cycle. Modification of RD-0233 including tank pressurization system. First flight 1974.
Status: Out of Production. Date: 1969-74. Thrust: 520.00 kN (116,900 lbf). Specific impulse: 310 s. Specific impulse sea level: 285 s. Burn time: 121 s.
Chamber Pressure: 205.00 bar.
Subtopics
| RD-0233 Kosberg N2O4/UDMH rocket engine. UR-100N / RS-18 (SS-19) stage 1. Out of Production. Staged combustion cycle. First flight 1974. |
| RD-0234-CH Kosberg LOx/LCH4 rocket engine. Developed 1996-. Proposed variant of RD-0234 engine using LOX-liquid methane instead of N2O4/UDMH as propellants. |
| RD-0234-HC Kosberg LOx/Kerosene rocket engine. Developed 1996-. Proposed variant of RD-0234 engine using LOX-kerosene instead of N2O4/UDMH as propellants. |
Family:
Storable liquid.
Country:
Russia.
Propellants:
N2O4/UDMH.
Stages:
UR-100N Stage 1N.
Agency:
Kosberg bureau.
Bibliography:
309,
339,
342,
353,
7487.
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