BA-44
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 restartable engine with composite ablative chamber and nozzle. Helium pressurant. Thrust declines to 50% of initial value before shutdown.
Throttled thrust(vac): 98.000 kN (22,031 lbf). Area Ratio: 100. Oxidizer to Fuel Ratio: 7.5. Restarts: 3.
Related
- Family
- Storable liquid
- Country
- USA
- Propellants
- H2O2/Kerosene
- Stages
- Beal BA-2 Stage 3
- Agency
- Beal
- Bibliography
- 455