LEADER 01683nam  2200493 a 450 
001 9910699506303321
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035   $a(CKB)5470000002403868
035   $a(OCoLC)679688941
035   $a(EXLCZ)995470000002403868
100   $a20101108d2010      ua             0
101 0 $aeng
135   $aurmn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aApproximate pressure distribution in an accelerating launch-vehicle fuel tank$b[electronic resource] /$fMichael P. Nemeth
210  1$aHampton, Va. :$cNational Aeronautics and Space Administration, Langley Research Center,$d[2010]
215   $a1 online resource (16 pages) $cillustrations
225 1 $aNASA/TM- ;$v2010-216681
300   $aTitle from title screen (viewed on Nov. 8, 2010).
300   $a"March 2010."
320   $aIncludes bibliographical references (page 8)
410  0$aNASA technical memorandum ;$v216681.
606   $aLiquid oxygen$2nasat
606   $aFuel tanks$2nasat
606   $aStructural design$2nasat
606   $aLaunch vehicles$2nasat
606   $aLiquid fuels$2nasat
606   $aPressure distribution$2nasat
615  7$aLiquid oxygen.
615  7$aFuel tanks.
615  7$aStructural design.
615  7$aLaunch vehicles.
615  7$aLiquid fuels.
615  7$aPressure distribution.
700   $aNemeth$b Michael P$01391721
712 02$aLangley Research Center.
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910699506303321
996   $aApproximate pressure distribution in an accelerating launch-vehicle fuel tank$93511793
997   $aUNINA