LEADER 00863nkm2-2200301---450- 001 990009997280403321 005 20150917105147.0 035 $a000999728 035 $aFED01000999728 035 $a(Aleph)000999728FED01 035 $a000999728 100 $a20150917f19601970km-y0itay50------ba 101 0 $ager 102 $aDE 116 $ahe-c-------------- 200 1 $aTarifa$bRisorsa grafica 210 $aBraunschweig$cGeorg Westermann Verlag$d[196.] 215 $a1 diapositiva$ccol.$d36 x 24 mm su supporto di cartone 50 x 50 mm 463 0$1001000999214 610 0 $aSpagna$aTarifa$aImmagini 710 02$aGeorg Westermann Verlag$0129269 801 0$aIT$bUNINA$gRICA$2UNIMARC 901 $aGR 912 $a990009997280403321 952 $aScat. West. O-02(016)$bIst. s.i.$fILFGE 959 $aILFGE 996 $aTarifa$91499503 997 $aUNINA LEADER 01701nam 2200445I 450 001 9910713543103321 005 20200526104420.0 035 $a(CKB)5470000002502233 035 $a(OCoLC)1155439734 035 $a(EXLCZ)995470000002502233 100 $a20200526j202004 ua 0 101 0 $aeng 135 $aur||||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aWind tunnel investigation of the supersonic stage separation aerodynamics of a generic 0.0175- scale bimese two-stage-to-orbit reusable launch vehicle configuration /$fGary E. Erickson 210 1$aHampton, Virginia :$cNational Aeronautics and Space Administration, Langley Research Center,$dApril 2020. 215 $a1 online resoure (iv, 545 pages, 1 unnumbered page) $cillustrations (chiefly color) 225 1 $aNASA/TM ;$v2020-220582 300 $a"April 2020." 320 $aIncludes bibliographical references (pages 38-40). 606 $aSupersonics$2nasat 606 $aWind tunnels$2nasat 606 $aShock waves$2nasat 606 $aBoundary layer separation$2nasat 606 $aStage separation$2nasat 615 7$aSupersonics. 615 7$aWind tunnels. 615 7$aShock waves. 615 7$aBoundary layer separation. 615 7$aStage separation. 700 $aErickson$b Gary E.$01403144 712 02$aLangley Research Center, 801 0$bGPO 801 1$bGPO 906 $aBOOK 912 $a9910713543103321 996 $aWind tunnel investigation of the supersonic stage separation aerodynamics of a generic 0.0175- scale bimese two-stage-to-orbit reusable launch vehicle configuration$93537022 997 $aUNINA