BA-810
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 50% of initial value before shutdown.
Throttled thrust(vac): 1,800.000 kN (404,600 lbf). Area Ratio: 25.13. Oxidizer to Fuel Ratio: 7.5.
Related
- Family
- Storable liquid
- Country
- USA
- Propellants
- H2O2/Kerosene
- Stages
- Beal BA-2 Stage 2
- Agency
- Beal
- Bibliography
- 455