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101 0 $aeng
135   $aur|||||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aAerodynamic stability characteristics of the Apollo command module /$fby William C. Moseley, Jr., Ralph E. Graham, and Jack E. Hughes
210  1$aWashington, D.C. :$cNational Aeronautics and Space Administration,$dAugust 1968.
215   $a1 online resource (xii, 171 pages) $cillustrations
225 1 $aNASA technical note ;$vTN D-4688
300   $a"August 1968."
320   $aIncludes bibliographical references (pages 15-16).
606   $aWind tunnel testing
606   $aSpace vehicles$xDesign and construction
606   $aStability of space vehicles
606   $aSpace vehicles$xDesign and construction$2fast
606   $aStability of space vehicles$2fast
606   $aWind tunnel testing$2fast
615  0$aWind tunnel testing.
615  0$aSpace vehicles$xDesign and construction.
615  0$aStability of space vehicles.
615  7$aSpace vehicles$xDesign and construction.
615  7$aStability of space vehicles.
615  7$aWind tunnel testing.
700   $aMoseley$b William C.$01420504
702   $aGraham$b Ralph E.
702   $aHughes$b Jack E.
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bOCLCE
801  1$bOCLCE
801  2$bOCLCQ
801  2$bOCLCF
801  2$bOCLCQ
801  2$bGPO
906   $aBOOK
912   $a9910715182103321
996   $aAerodynamic stability characteristics of the Apollo command module$93538526
997   $aUNINA