LEADER 01749nam  2200457   450 
001 9910707968003321
005 20170126153553.0
035   $a(CKB)5470000002468887
035   $a(OCoLC)970348771
035   $a(EXLCZ)995470000002468887
100   $a20170126j201607    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aDevelopment of constraint force equation methodology for application to multi-body dynamics including launch vehicle stage separation /$fBandu N. Pamadi [and five others]
210  1$aHampton, Virginia :$cNational Aeronautics and Space Administration, Langley Research Center,$dJuly 2016.
215   $a1 online resource (xvi, 112 pages) $cillustrations
225 1 $aNASA/TP ;$v2016-219326
300   $a"July 2016."
300   $a"Performing organization: NASA Langley Research Center"--Report documentation page.
320   $aIncludes bibliographical references (pages 111-112).
606   $aAerodynamic forces$2nasat
606   $aBooster rocket engines$2nasat
606   $aLaunch vehicles$2nasat
606   $aOrbit insertion$2nasat
606   $aStage separation$2nasat
615  7$aAerodynamic forces.
615  7$aBooster rocket engines.
615  7$aLaunch vehicles.
615  7$aOrbit insertion.
615  7$aStage separation.
700   $aPamadi$b Bandu N.$f1945-$0727368
712 02$aLangley Research Center,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910707968003321
996   $aDevelopment of constraint force equation methodology for application to multi-body dynamics including launch vehicle stage separation$93520261
997   $aUNINA