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Castor 4B
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Gross Mass: 11,400 kg (25,100 lb). Empty Mass: 1,400 kg (3,000 lb). Thrust (vac): 430.610 kN (96,805 lbf). Isp: 281 sec. Burn time: 64 sec. Propellants: Solid. Isp(sl): 220 sec. Diameter: 1.02 m (3.34 ft). Span: 1.02 m (3.34 ft). Length: 9.20 m (30.10 ft). Country: USA. No Engines: 1. Engine: Castor 4B. Status: Out of production. Cost $ : 2.500 million. First Flight: 1982. Last Flight: 1982. No Launched: 3. Optimized for high altitude (Conestoga)
Used on Launch Vehicles:
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© Mark Wade, 1997 - 2007 except where otherwise noted.
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