BA-3200
Engine · USA
Original archive entry. The text, images and links below are kept as they were written.
Beal H2O2/Kerosene rocket engine. Development 1990's. Pressure-fed engine with composite ablative chamber and nozzle. Helium pressurant. Thrust declines to 70% of initial value before shutdown.
Throttled thrust(vac): 9,870.000 kN (2,218,860 lbf). Area Ratio: 6.48. Oxidizer to Fuel Ratio: 7.
Related
- Family
- Storable liquid
- Country
- USA
- Propellants
- H2O2/Kerosene
- Stages
- Beal BA-2 Stage 1
- Agency
- Beal
- Bibliography
- 455