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
Vexin A
Number: 44 . Thrust: 68.60 kN (15,422 lbf). Unfuelled mass: 175 kg (385 lb). Specific impulse: 277 s. Specific impulse sea level: 240 s. Burn time: 96 s. Diameter: 0.50 m (1.64 ft).
Thrust (sl): 59.500 kN (13,376 lbf). Thrust (sl): 6,065 kgf. Engine: 175 kg (385 lb). Thrust to Weight Ratio: 40.
| Europa-2 N2O4/UDMH propellant rocket stage. . |
| Diamant B-1 N2O4/UDMH propellant rocket stage. . |
| Diamant-1 N2O4/UDMH propellant rocket stage. . |
| Vexin B SEP N2O4/UDMH rocket engine. Out of production. Used on Diamant launch vehicle. First flight 1965. |
| Vexin C SEP N2O4/UDMH rocket engine. Out of production. Used on Diamant B launch vehicle. First flight 1970. |
Family: Storable liquid. Country: France. Launch Vehicles: Europa I. Propellants: N2O4/UDMH. Stages: Europa-2.
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