LEADER 01907oam  2200517I  450 
001 9910707239603321
005 20160621154007.0
035   $a(CKB)5470000002463113
035   $a(OCoLC)227848727
035   $a(EXLCZ)995470000002463113
100   $a20080512j199612    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aComparison of separation shock for explosive and nonexplosive release actuators on a small spacecraft panel /$fM.H. Lucy and R.D. Buehrle, J.P. Woolley
210  1$aHampton, Virginia :$cNational Aeronautics and Space Administration, Langley Research Center,$dDecember 1996.
215   $a1 online resource (i, 50 pages)$cillustrations
225 1 $aNASA technical memorandum ;$v110257
300   $aTitle from title screen (viewed June 20, 2016).
300   $a"December 1996."
300   $a"Performing organization: NASA Langley Research Center, Hampton, VA"--Report documentation page.
606   $aSpacecraft design$2nasat
606   $aBooster rocket engines$2nasat
606   $aActuators$2nasat
606   $aShock spectra$2nasat
606   $aStage separation$2nasat
615  7$aSpacecraft design.
615  7$aBooster rocket engines.
615  7$aActuators.
615  7$aShock spectra.
615  7$aStage separation.
700   $aLucy$b M. H.$01387210
702   $aBuehrle$b Ralph D$g(Ralph David),
702   $aWoolley$b J. P.
712 02$aLangley Research Center,
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bDTICE
801  1$bDTICE
801  2$bOCLCQ
801  2$bGPO
906   $aBOOK
912   $a9910707239603321
996   $aComparison of separation shock for explosive and nonexplosive release actuators on a small spacecraft panel$93436789
997   $aUNINA