LEADER 02078oam 2200613I 450 001 9910713907303321 005 20201211085751.0 035 $a(CKB)5470000002506594 035 $a(OCoLC)761203525 035 $a(EXLCZ)995470000002506594 100 $a20111115j196903 ua 0 101 0 $aeng 135 $aur||||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aEffects of bottom-structure flexibility on water landing loads of Apollo spacecraft models /$fby Sandy M. Stubbs and Melvin E. Hathaway 210 1$aWashington, D.C. :$cNational Aeronautics and Space Administration,$dMarch 1969. 215 $a1 online resource (30 pages) $cillustrations 225 1 $aNASA technical note ;$vNASA TN D-5108 300 $a"March 1969." 320 $aIncludes bibliographical references (page 11). 606 $aSpace vehicles$xLanding 606 $aImpact 606 $aShielding (Heat)$xMaterials$xTesting 606 $aMaterials$xDynamic testing 606 $aImpact$2fast 606 $aMaterials$xDynamic testing$2fast 606 $aShielding (Heat)$xMaterials$xTesting$2fast 606 $aSpace vehicles$xLanding$2fast 615 0$aSpace vehicles$xLanding. 615 0$aImpact. 615 0$aShielding (Heat)$xMaterials$xTesting. 615 0$aMaterials$xDynamic testing. 615 7$aImpact. 615 7$aMaterials$xDynamic testing. 615 7$aShielding (Heat)$xMaterials$xTesting. 615 7$aSpace vehicles$xLanding. 700 $aStubbs$b Sandy M.$01420794 702 $aHathaway$b Melvin E. 712 02$aUnited States.$bNational Aeronautics and Space Administration, 712 02$aLangley Research Center. 801 0$bOCLCE 801 1$bOCLCE 801 2$bOCLCQ 801 2$bOCLCF 801 2$bOCLCQ 801 2$bCOP 801 2$bOCLCO 801 2$bGPO 906 $aBOOK 912 $a9910713907303321 996 $aEffects of bottom-structure flexibility on water landing loads of Apollo spacecraft models$93539961 997 $aUNINA