LEADER 01817nam  2200493I  450 
001 9910703640803321
005 20150807154404.0
035   $a(CKB)5470000002433304
035   $a(OCoLC)916509991
035   $a(EXLCZ)995470000002433304
100   $a20150807j201402    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aPressure-volume-temperature (PVT) gauging of an isothermal cryogenic propellant tank pressurized with gaseous helium /$fNeil T. Van Dresar and Gregory A. Zimmerli
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$dFebruary 2014.
215   $a1 online resource (23 pages) $cillustrations
225 1 $aNASA/TP ;$v2014-218083
300   $aTitle from title screen (viewed Aug. 7, 2015).
300   $a"February 2014."
320   $aIncludes bibliographical references (page 23).
517   $aPressure-volume-temperature 
606   $aPropellant tanks$2nasat
606   $aLiquid oxygen$2nasat
606   $aLiquid nitrogen$2nasat
606   $aHelium$2nasat
606   $aFuel tank pressurization$2nasat
615  7$aPropellant tanks.
615  7$aLiquid oxygen.
615  7$aLiquid nitrogen.
615  7$aHelium.
615  7$aFuel tank pressurization.
700   $aVan Dresar$b Neil T.$01407461
702   $aZimmerli$b Gregory A.
712 02$aNASA Glenn Research Center,
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910703640803321
996   $aPressure-volume-temperature (PVT) gauging of an isothermal cryogenic propellant tank pressurized with gaseous helium$93541499
997   $aUNINA