LEADER 01636nam  2200469   450 
001 9910709750603321
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035   $a(OCoLC)1042243356
035   $a(EXLCZ)995470000002472740
100   $a20180629j198211    ua             0
101 0 $aeng
135   $aur|||||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aComputer program for post-flight analysis of rigid body moments acting on a launch vehicle first stage /$fR.N. Knauber
210  1$aHampton, Virginia :$cNational Aeronautics and Space Administration, Langley Research Center,$dNovember 1982.
215   $a1 online resource (ix, 111 pages) $cillustrations
225 1 $aNASA/CR ;$v166033
300   $a"November 1982."
300   $aIncludes appendix.
320   $aIncludes bibliographical references (page 41).
606   $aComputer programs$2nasat
606   $aPostflight analysis$2nasat
606   $aLaunch vehicles$2nasat
606   $aAerodynamic coefficients$2nasat
606   $aRigid structures$2nasat
615  7$aComputer programs.
615  7$aPostflight analysis.
615  7$aLaunch vehicles.
615  7$aAerodynamic coefficients.
615  7$aRigid structures.
700   $aKnauber$b R. N.$01391888
712 02$aLangley Research Center,
712 02$aVought Corporation.
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910709750603321
996   $aComputer program for post-flight analysis of rigid body moments acting on a launch vehicle first stage$93445979
997   $aUNINA