H1500 Propellants: Lox/Solid. Thrust(vac): 931.300 kN (209,365 lbf). Thrust(sl): 928.000 kN (208,622 lbf). Isp: 284 sec. Isp (sea level): 283 sec. Burn time: 75 sec. Diameter: 1.83 m (6.00 ft). Chambers: 1. Country: USA. Status: Design 1988. H1500 used on Rocket Stages Used on stage: AMROC. on launch vehicle: Industrial Launch Vehicle. Used on stage: AMROC. on launch vehicle: Industrial Launch Vehicle. Used on stage: AMROC. on launch vehicle: Industrial Launch Vehicle. Used on stage: AMROC. on launch vehicle: Industrial Launch Vehicle.                   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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