Aerobee 150A-2

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Aerobee 150A-2

Part of AJ11 engine series

Aerojet ntric acid/Amine propellant rocket stage. Typical ideal dV=3839 m/s; gravity and drag losses = 1012 m/s.

AKA: AJ11-21. Status: Retired 1973. Thrust: 18.24 kN (4,101 lbf). Gross mass: 611 kg (1,347 lb). Unfuelled mass: 133 kg (293 lb). Specific impulse: 209 s. Specific impulse sea level: 209 s. Burn time: 51 s. Height: 5.10 m (16.70 ft). Diameter: 0.38 m (1.24 ft).

Nitric acid/Aniline engine.

Family: Storable liquid. Country: USA. Engines: AJ11-6. Launch Vehicles: Aerobee 150A. Propellants: Nitric acid/Amine. Agency: Aerojet.

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