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001 9910707496903321
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100   $a20160809j199701    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 12$aA rocket engine for Mars sample return using in situ propellants /$fDiane L. Linne
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Lewis Research Center,$dJanuary 1997.
215   $a1 online resource (10 pages) $cillustrations
225 1 $aNASA technical memorandum ;$v107396
300   $aTitle from title screen (viewed Aug. 9, 2016).
300   $a"January 1997"--Report documentation page.
300   $a"Prepared for the 35th Aerospace Sciences Meeting and Exhibit cosponsored by AIAA, ASME, SAE, and ASME, Reno, Nevada, January 6-10, 1997."
300   $a"Performing organization: National Aeronautics and Space Administration, Lewis Research Center"--Report documentation page.
300   $a"AIAA-97-0893."
320   $aIncludes bibliographical references (pages 9-10).
606   $aCarbon monoxide$2nasat
606   $aRocket engines$2nasat
606   $aEngine design$2nasat
606   $aPropulsion system performance$2nasat
606   $aRocket propellants$2nasat
606   $aRefractory materials$2nasat
606   $aCeramic matrix composites$2nasat
615  7$aCarbon monoxide.
615  7$aRocket engines.
615  7$aEngine design.
615  7$aPropulsion system performance.
615  7$aRocket propellants.
615  7$aRefractory materials.
615  7$aCeramic matrix composites.
700   $aLinne$b Diane L.$01403191
712 02$aLewis Research Center,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910707496903321
996   $aA rocket engine for Mars sample return using in situ propellants$93514646
997   $aUNINA