2.5KS18000

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Model: Aerobee 300A-1. Gross Mass: 272 kg (599 lb). Empty Mass: 153 kg (337 lb). Thrust (vac): 80.000 kN (17,984 lbf). Burn time: 2.50 sec. Propellants: Solid. Isp(sl): 167 sec. Diameter: 0.33 m (1.08 ft). Length: 1.80 m (5.90 ft). Country: USA. No Engines: 1. Motor: 2.5KS18000. Status: Retired 1985. First Flight: 1947. Last Flight: 1983. No Launched: 813. Used as: Aerobee Booster.

Typical ideal dV=259 m/s; gravity and drag losses = 25 m/s.

Model: Aerobee 150A MII-1. Gross Mass: 300 kg (660 lb). Empty Mass: 140 kg (300 lb). Thrust (vac): 80.000 kN (17,984 lbf). Burn time: 2.50 sec. Propellants: Solid. Diameter: 0.33 m (1.08 ft). Length: 1.80 m (5.90 ft). Country: USA. No Engines: 1. Motor: 2.5KS18000. Status: Retired 1985. First Flight: 1968. Last Flight: 1985. No Launched: 20. Used as: Aerobee Booster.

Model: Aerobee 150 MII 20-1. Gross Mass: 300 kg (660 lb). Empty Mass: 140 kg (300 lb). Thrust (vac): 80.000 kN (17,984 lbf). Burn time: 2.50 sec. Propellants: Solid. Diameter: 0.33 m (1.08 ft). Length: 1.80 m (5.90 ft). Country: USA. No Engines: 1. Motor: 2.5KS18000. Status: Retired 1970. First Flight: 1970. Last Flight: 1970. No Launched: 1. Used as: Aerobee Booster.

Used on Launch Vehicles:

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