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Aerobee 150-2
Nitric acid/Aniline propellant rocket stage. Thrust 17.80 kN.

AKA: Aerobee. Status: Retired 1985. Thrust: 17.80 kN (4,002 lbf). Gross mass: 700 kg (1,540 lb). Unfuelled mass: 133 kg (293 lb). Burn time: 51 s. Height: 5.10 m (16.70 ft). Diameter: 0.38 m (1.24 ft).

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Aerobee 150A-2 Nitric acid/Amine propellant rocket stage. Nitric acid/Aniline propellants. Typical ideal dV=3839 m/s; gravity and drag losses = 1012 m/s.

Country: USA. Engines: AJ11-6. Launch Vehicles: Aerobee Hi, Aerobee, Aerobee 300, Aerobee 150, Aerobee 300A, Aerobee 150 MI, Aerobee 170, Aerobee 170B, Aerobee 170A, Aerobee 150A MII. Propellants: Nitric acid/Amine. Agency: Aerojet.

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