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Atlas V SRB
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Gross Mass: 40,824 kg (90,001 lb). Empty Mass: 4,000 kg (8,800 lb). Thrust (vac): 1,270.000 kN (285,500 lbf). Isp: 275 sec. Burn time: 94 sec. Propellants: Solid. Isp(sl): 245 sec. Diameter: 1.55 m (5.08 ft). Span: 1.00 m (3.20 ft). Length: 17.70 m (58.00 ft). Country: USA. No Engines: 1. Engine: Aerojet SRB. Status: In production. First Flight: 2002. Last Flight: 2006. No Launched: 40. New SRB boosters in development for Atlas V. Empty mass, vacuum thrust, sea level Isp estimated.
Used on Launch Vehicles:
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© Mark Wade, 1997 - 2007 except where otherwise noted.
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