HYSR

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Model: HYSR-1. Thrust (vac): 270.000 kN (60,690 lbf). Propellants: Lox/Solid. Diameter: 0.61 m (2.00 ft). Length: 15.00 m (49.00 ft). Country: USA. No Engines: 1. Motor: HYSR. Status: Retired 2002. Used as: HYSR. Release conditions: LMSS. Used on Launch Vehicles: HYSR. 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.