H2O2/Kerosene propellant rocket stage. Loaded/empty mass 189,000/14,560 kg. Thrust 3,599.00 kN. Vacuum specific impulse 282 seconds. Thrust declines to 50% of initial value at shut down.
Status: Development 2000.
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Gross mass: 189,000 kg (416,000 lb).
Unfuelled mass: 14,560 kg (32,090 lb).
Height: 18.80 m (61.60 ft).
Diameter: 6.20 m (20.30 ft).
Span: 6.20 m (20.30 ft).
Thrust: 3,599.00 kN (809,087 lbf).
Specific impulse: 282 s.
Burn time: 168 s.
BA-810 Beal H2O2/Kerosene rocket engine. 3600 kN. Development 1990's. Pressure-fed engine with composite ablative chamber and nozzle. Helium pressurant. Thrust declines to 50% of initial value before shutdown. Isp=282s. 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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