| Atlas V SRB |
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Model: Atlas V SRB. 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. Motor: Aerojet SRB. Status: Active. First Flight: 2003. Last Flight: 2006. No Launched: 14. New SRB boosters in development for Atlas V. Empty mass, vacuum thrust, sea level Isp estimated. Used on Launch Vehicles: Contact us with any corrections, additions, or comments. Conditions for use of drawings, pictures, or other materials from this site.. To contact astronauts or cosmonauts. © Mark Wade, 1997 - 2008 except where otherwise noted. |