LEADER 01666oam 2200481 450 001 9910715035703321 005 20201123132410.0 035 $a(CKB)5470000002507649 035 $a(OCoLC)761182057 035 $a(EXLCZ)995470000002507649 100 $a20111115j196808 ua 0 101 0 $aeng 135 $aur||||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aFlight-test analysis of Apollo heat-shield material using the pacemaker vehicle system /$fby Randolph A. Graves, Jr., William G. Witte 210 1$aWashington, D.C. :$cNational Aeronautics and Space Administration,$dAugust 1968. 215 $a1 online resource (34 pages) $cillustrations 225 1 $aNASA technical note ;$vTN D-4713 300 $a"August 1968." 320 $aIncludes bibliographical references (pages 15-16). 606 $aSpace vehicles$xShielding (Heat)$xTesting 606 $aNoses (Space vehicles) 606 $aNoses (Space vehicles)$2fast 615 0$aSpace vehicles$xShielding (Heat)$xTesting. 615 0$aNoses (Space vehicles) 615 7$aNoses (Space vehicles) 700 $aGraves$b Randolph A.$01416784 702 $aWitte$b William G. 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$bOCLCO 801 2$bOCLCQ 801 2$bOCLCF 801 2$bGPO 906 $aBOOK 912 $a9910715035703321 996 $aFlight-test analysis of Apollo heat-shield material using the pacemaker vehicle system$93523326 997 $aUNINA