AMROC IRR

home topic index

Model: AMROC IRR. Gross Mass: 12,200 kg (26,800 lb). Thrust (vac): 315.000 kN (70,814 lbf). Burn time: 70 sec. Propellants: Lox/Solid. Diameter: 1.29 m (4.23 ft). Length: 17.70 m (58.00 ft). Country: USA. No Engines: 1. Motor: H1500. Status: Retired 1989. First Flight: 1989. Last Flight: 1989. No Launched: 1. Used as: AMROC. Other designations: IRR. Release conditions: AMROC. Used on Launch Vehicles: AMROC. 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.