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2.5KS18000
Multiple-source solid rocket engine. Typical ideal dV=259 m/s; gravity and drag losses = 25 m/s.

AKA: Aerobee 150 MII 20-1;Aerobee 150A MII-1;Aerobee 300A-1. Status: Retired 1985. Thrust: 80.00 kN (17,984 lbf). Gross mass: 272 kg (599 lb). Unfuelled mass: 153 kg (337 lb). Burn time: 2.50 s. Height: 1.80 m (5.90 ft). Diameter: 0.33 m (1.08 ft).



Country: USA. Launch Vehicles: Aerobee RTV-N-8, Aerobee XASR-SC-1, Aerobee RTV-A-1, Aerobee RTV-N-10, Aerobee XASR-SC-2, Aerobee RTV-A-1b, Aerobee RTV-A-1a, Aerobee RTV-N-10b, Aerobee RTV-N-10c, Aerobee Hi, Aerobee AJ10-27, Aerobee RTV-N-10a, Aerobee AJ10-34, Aerobee AJ10-25, Aerobee, Aerobee 100, Aerobee 300, Aerobee 150, Aerobee 150A, Aerobee 300A, Aerobee 150 MI, Aerobee 150A MII. Propellants: Solid. Stages: 2.5KS18000.

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