XASR-1

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Engine Model: XASR-1. Designer: Aerojet. Propellants: Nitric acid/aniline. Thrust(vac): 11.600 kN (2,608 lbf). Burn time: 32 sec. Country: USA. XASR-1 used on Rocket Stages Used on stage: Aerobee. on launch vehicle: Aerobee. 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.