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035   $a(OCoLC)954603898
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100   $a20160803j199612    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aDesign factors for applying cryogen storage and delivery technology to solar thermal propulsion /$fMarc G. Millis
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Lewis Research Center,$dDecember 1996.
215   $a1 online resource (6 pages) $cillustrations
225 1 $aNASA technical memorandum ;$v107379
300   $aTitle from title screen (viewed Aug. 3, 2016).
300   $a"December 1996"--Report documentation page.
300   $a"Prepared for the Space Technology and Applications International Forum cosponsored by NASA, DSWA, U.S. DOE, and USAF, Albuquerque, New Mexico, January 26-30, 1997."
300   $a"Performing organization: National Aeronautics and Space Administration, Lewis Research Center"--Report documentation page.
320   $aIncludes bibliographical references (pages 5-6).
606   $aSolar thermal propulsion$2nasat
606   $aPropellant storage$2nasat
606   $aMultilayer insulation$2nasat
606   $aMicrogravity$2nasat
606   $aCryogenics$2nasat
606   $aSpacecraft propulsion$2nasat
606   $aLiquid hydrogen$2nasat
615  7$aSolar thermal propulsion.
615  7$aPropellant storage.
615  7$aMultilayer insulation.
615  7$aMicrogravity.
615  7$aCryogenics.
615  7$aSpacecraft propulsion.
615  7$aLiquid hydrogen.
700   $aMillis$b Marc G.$01088592
712 02$aLewis Research Center,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910707308303321
996   $aDesign factors for applying cryogen storage and delivery technology to solar thermal propulsion$93487270
997   $aUNINA