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BA-44
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.

Status: Development 1990's. Thrust: 196.00 kN (44,062 lbf). Specific impulse: 300 s. Burn time: 600 s.

Throttled thrust(vac): 98.000 kN (22,031 lbf). Area Ratio: 100. Oxidizer to Fuel Ratio: 7.5. Restarts: 3.



Family: Storable liquid. Country: USA. Propellants: H2O2/Kerosene. Stages: Beal BA-2 Stage 3. Agency: Beal. Bibliography: 455.

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