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Aerojet SRB
Aerojet solid rocket engine. In production. First flight 2002. Solid propellant rocket stage. SRB boosters for Atlas V. Empty mass, vacuum thrust, sea level Isp estimated.

AKA: Atlas V SRB. Status: In production. Date: 1996-2002. Number: 40 . Thrust: 1,270.00 kN (285,500 lbf). Gross mass: 40,824 kg (90,001 lb). Unfuelled mass: 4,000 kg (8,800 lb). Specific impulse: 275 s. Specific impulse sea level: 245 s. Burn time: 94 s. Height: 17.70 m (58.00 ft). Diameter: 1.55 m (5.08 ft).

Country: USA. Launch Vehicles: Atlas V 521, Atlas V 431, Atlas V 411, Atlas V 501. Propellants: Solid. Stages: Aerojet SRB. Agency: Aerojet.



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