01785oam 2200505I 450 991071407160332120201106104822.0(CKB)5470000002506928(OCoLC)890695707(EXLCZ)99547000000250692820140916j196810 ua 0engur|||||||||||txtrdacontentcrdamediacrrdacarrierEffect of thrust per element on combustion stability characteristics of hydrogen-oxygen rocket engines /by Reino J. Salmi, John P. Wanhainen, and Ned P. HannumWashington, D.C. :National Aeronautics and Space Administration,October 1968.1 online resource (ii, 27 pages) illustrationsNASA technical note ;TN D-4851"October 1968."Includes bibliographical references (pages 26-27).Rocket enginesCombustionRocket enginesThrustRocket enginesCombustionfastRocket enginesThrustfastRocket enginesCombustion.Rocket enginesThrust.Rocket enginesCombustion.Rocket enginesThrust.Salmi Reino J.1395045Wanhainen John P.Hannum Ned P.United States.National Aeronautics and Space Administration,Lewis Research Center.OCLCEOCLCEOCLCOOCLCQOCLCFGPOBOOK9910714071603321Effect of thrust per element on combustion stability characteristics of hydrogen-oxygen rocket engines3453007UNINA