Ariane 5-0 P230
Engine · France
Original archive entry. The text, images and links below are kept as they were written.
SNPE solid rocket engine. In production. Used on Ariane 5 launch vehicle. First flight 1996. Solid propellant rocket stage. Solid rocket booster for Ariane 5. Nozzle expansion ratio increased from 9.7 to 11.0 after 1997. Chamber pressure 61.3 bar. HTPB propellant.
SNPE solid rocket engine. In production. Used on Ariane 5 launch vehicle. First flight 1996. Solid propellant rocket stage. Solid rocket booster for Ariane 5. Nozzle expansion ratio increased from 9.7 to 11.0 after 1997. Chamber pressure 61.3 bar. HTPB propellant. Ariane 5 zero stage.
Subtopics
- Ariane 5-0 P241 SEP solid rocket engine. First flight 2002. Solid propellant rocket stage. Increased propellant loading (+2.43 metric tons), lighter welded case (-1.6 metric tons) compared to earlier versions.
Related
- Country
- France
- Launch Vehicles
- Ariane 5, Ariane 5G, Ariane 5Gp, Ariane 5GS
- Propellants
- Solid
- Stages
- Ariane 5-0 P230
- Agency
- SNPE