Aerojet SRB Designer: Aerojet. Developed in: 1996-2002. Gross Mass: 40,824 kg (90,001 lb). Empty Mass: 4,000 kg (8,800 lb). Propellants: Solid. Thrust(vac): 1,270.000 kN (285,500 lbf). Isp: 275 sec. Isp (sea level): 245 sec. Burn time: 94 sec. Diameter: 1.55 m (5.08 ft). Length: 17.70 m (58.00 ft). Chambers: 1. Country: USA. Status: In production. First Flight: 2002. Last Flight: 2006. Flown: 40. Aerojet SRB used on Rocket Stages Used on stage: Atlas V SRB. on launch vehicle: Atlas V.                   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 - 2007 except where otherwise noted.

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