LEADER 01983nam  2200553I  450 
001 9910704629003321
005 20130705143034.0
035   $a(CKB)5470000002443427
035   $a(OCoLC)851800599
035   $a(EXLCZ)995470000002443427
100   $a20130705d2013      ua             0
101 0 $aeng
135   $aurmn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aLarge-scale liquid hydrogen tank rapid chill and fill testing for the advanced shuttle upper stage concept /$fR.H. Flachbart [and six others]
210  1$aHuntsville, Alabama :$cNational Aeronautics and Space Administration, Marshall Space Flight Center,$d2013.
215   $a1 online resource (vii, 43 pages) $cillustrations (some color)
225 1 $aNASA/TP ;$v2013-217482
300   $aTitle from title screen (viewed on July 5, 2013).
300   $a"April 2013."
320   $aIncludes bibliographical references (page 43).
606   $aUpper stage rocket engines$2nasat
606   $aCryogenic fluids$2nasat
606   $aFluid management$2nasat
606   $aLiquid hydrogen$2nasat
606   $aFilm boiling$2nasat
606   $aHeat transfer$2nasat
606   $aCryogenic cooling$2nasat
606   $aPropellant tanks$2nasat
606   $aFuel tank pressurization$2nasat
615  7$aUpper stage rocket engines.
615  7$aCryogenic fluids.
615  7$aFluid management.
615  7$aLiquid hydrogen.
615  7$aFilm boiling.
615  7$aHeat transfer.
615  7$aCryogenic cooling.
615  7$aPropellant tanks.
615  7$aFuel tank pressurization.
700   $aFlachbart$b R. H.$01418319
712 02$aGeorge C. Marshall Space Flight Center,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910704629003321
996   $aLarge-scale liquid hydrogen tank rapid chill and fill testing for the advanced shuttle upper stage concept$93529394
997   $aUNINA