HYSR

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Engine Model: HYSR. Designer: LMSS. Propellants: Lox/Solid. Thrust(vac): 270.000 kN (60,690 lbf). Country: USA. HYSR used on Rocket Stages Used on stage: HYSR. on launch vehicle: 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.