LEADER 01905nam  2200541   450 
001 9910703411403321
005 20150130105206.0
035   $a(CKB)5470000002431581
035   $a(OCoLC)901411946
035   $a(EXLCZ)995470000002431581
100   $a20150130j201311    ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aMars sample return$eMars Ascent Vehicle mission & technology requirements /$fJeffrey V. Bowles [and three others]
205   $aRevA.
210  1$aMoffett Field, CA :$cNational Aeronautics and Space Administration, Ames Research Center,$dNovember 2013.
215   $a1 online resource (54 pages) $ccolor illustrations
225 1 $aNASA/TM ;$v2013-216620
300   $aTitle from title screen (viewed on Jan. 30, 2015).
300   $a"November 2013."
300   $aThis document completely replaces NASA/TM-2013-216511.
320   $aIncludes bibliographical references (page 54).
517   $aMars sample return 
606   $aMars sample return missions$2nasat
606   $aSpacecraft propulsion$2nasat
606   $aMars landing$2nasat
606   $aReturn to Earth space flight$2nasat
606   $aAscent trajectories$2nasat
606   $aComputational fluid dynamics$2nasat
606   $aHypergolic rocket propellants$2nasat
615  7$aMars sample return missions.
615  7$aSpacecraft propulsion.
615  7$aMars landing.
615  7$aReturn to Earth space flight.
615  7$aAscent trajectories.
615  7$aComputational fluid dynamics.
615  7$aHypergolic rocket propellants.
700   $aBowles$b Jeffrey V.$01390947
712 02$aAmes Research Center,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910703411403321
996   $aMars sample return$93444141
997   $aUNINA