01701nam 2200445I 450 991071354310332120200526104420.0(CKB)5470000002502233(OCoLC)1155439734(EXLCZ)99547000000250223320200526j202004 ua 0engur|||||||||||txtrdacontentcrdamediacrrdacarrierWind tunnel investigation of the supersonic stage separation aerodynamics of a generic 0.0175- scale bimese two-stage-to-orbit reusable launch vehicle configuration /Gary E. EricksonHampton, Virginia :National Aeronautics and Space Administration, Langley Research Center,April 2020.1 online resoure (iv, 545 pages, 1 unnumbered page) illustrations (chiefly color)NASA/TM ;2020-220582"April 2020."Includes bibliographical references (pages 38-40).SupersonicsnasatWind tunnelsnasatShock wavesnasatBoundary layer separationnasatStage separationnasatSupersonics.Wind tunnels.Shock waves.Boundary layer separation.Stage separation.Erickson Gary E.1403144Langley Research Center,GPOGPOBOOK9910713543103321Wind tunnel investigation of the supersonic stage separation aerodynamics of a generic 0.0175- scale bimese two-stage-to-orbit reusable launch vehicle configuration3537022UNINA