|
Engine Model: 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
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.
|
|