Encyclopedia Astronautica 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-0124-14D23 AKA: 14D23. Status: Designed 1986-1990. Thrust: 298.64 kN (67,137 lbf). Specific impulse: 331 s. Burn time: 300 s. Proposed for small launcher Kvant-1 by RKK Energia for stage 1 steering engine. Also proposed by RKK Energia in initial studies in 1993 for Angara upper stage.
Chambers: 4. Chamber Pressure: 173.50 bar. Oxidizer to Fuel Ratio: 2.6.
Country: Russia. Launch Vehicles: Kvant-1. Propellants: Lox/Kerosene. Stages: Kvant-1-1. Agency: Kosberg bureau. Bibliography: 21, 312. 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 � 1997-2016 Mark Wade - Contact � / Conditions for Use |
