H2O2/Kerosene propellant rocket stage. Loaded/empty mass 36,700/2,855 kg. Thrust 196.00 kN. Vacuum specific impulse 300 seconds. Thrust declines to 50% of initial value at shut down.
Status: Development 2000.
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Gross mass: 36,700 kg (80,900 lb).
Unfuelled mass: 2,855 kg (6,294 lb).
Height: 8.20 m (26.90 ft).
Diameter: 6.20 m (20.30 ft).
Span: 6.20 m (20.30 ft).
Thrust: 196.00 kN (44,062 lbf).
Specific impulse: 300 s.
Burn time: 600 s.
BA-44 Beal H2O2/Kerosene rocket engine. 196 kN. Development 1990's. Pressure-fed restartable engine with composite ablative chamber and nozzle. Helium pressurant. Thrust declines to 50% of initial value before shutdown. Isp=300s. More...
H2O2/Kerosene Hydrogen peroxide is used as both an oxidiser and a monopropellant. Relatively high density and non-toxic, it was abandoned after early use in British rockets, but recently revived as a propellant for the Black Horse spaceplane. Rocket propellant RP-1, or its foreign equivalents, is a straight-run kerosene fraction, which is subjected to further treatment, i.e., acid washing, sulphur dioxide extraction. Thus, unsaturated substances which polymerise in storage are removed, as are sulphur-containing hydrocarbons. More...
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