LEADER 01934nam 2200505Ia 450 001 9910700710303321 005 20111014122815.0 035 $a(CKB)5470000002411908 035 $a(OCoLC)756924215 035 $a(EXLCZ)995470000002411908 100 $a20111014d2011 ua 0 101 0 $aeng 135 $aurcn||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 00$aEnabling long-duration lunar equatorial operations with thermal wadi infrastructure$b[electronic resource] /$fHeather L. Jones ... [and others] ; prepared for the 49th Aerospace Sciences Meeting sponsored by the American Institute of Aeronautics and Astronautics, Orlando, Florida, January 4-7, 2011 210 1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$d[2011] 215 $a1 online resource (13 pages) $ccolor illustrations 225 1 $aNASA/TM ;$v2011-216994 300 $aTitle from title screen (viewed on Oct. 14, 2011). 300 $a"March 2011." 300 $a"AIAA-2011-0703." 320 $aIncludes bibliographical references (page 13). 606 $aRoving vehicles$2nasat 606 $aRobotics$2nasat 606 $aSolar generators$2nasat 606 $aCryogenic temperature$2nasat 606 $aHeat sources$2nasat 606 $aLunar surface$2nasat 615 7$aRoving vehicles. 615 7$aRobotics. 615 7$aSolar generators. 615 7$aCryogenic temperature. 615 7$aHeat sources. 615 7$aLunar surface. 701 $aJones$b Heather L$01395869 712 02$aNASA Glenn Research Center. 712 12$aAIAA Aerospace Sciences Meeting$d(49th :$f2011 :$eOrlando, Fla.) 801 0$bGPO 801 1$bGPO 906 $aBOOK 912 $a9910700710303321 996 $aEnabling long-duration lunar equatorial operations with thermal wadi infrastructure$93455048 997 $aUNINA LEADER 02021oam 2200541 450 001 9910707804103321 005 20170111112438.0 035 $a(CKB)5470000002468522 035 $a(OCoLC)761261209 035 $a(EXLCZ)995470000002468522 100 $a20111115j198711 ua 0 101 0 $aeng 135 $aurbn||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aIntegration effects of D-shaped, underwing, aft-mounted, separate-flow, flow-through nacelles on a high-wing transport /$fMilton Lamb, John R. Carlson, and Odis C. Pendergraft 210 1$aWashington, D.C. :$cNational Aeronautics and Space Administration, Scientific and Technical Information Division,$dNovember 1987. 215 $a1 online resource (21 pages) $cillustrations 225 1 $aNASA technical memorandum ;$v4018 300 $a"November 1987." 300 $a"Performing organization: NASA Langley Research Center"--Report documentation page. 320 $aIncludes bibliographical references (page 3). 606 $aAngle of attack$2nasat 606 $aNacelles$2nasat 606 $aSeparated flow$2nasat 606 $aSupersonic flow$2nasat 606 $aTransonic wind tunnels$2nasat 615 7$aAngle of attack. 615 7$aNacelles. 615 7$aSeparated flow. 615 7$aSupersonic flow. 615 7$aTransonic wind tunnels. 700 $aLamb$b Milton$01393161 702 $aCarlson$b John R. 702 $aPendergraft$b Odis C. 712 02$aLangley Research Center. 712 02$aUnited States.$bNational Aeronautics and Space Administration.$bScientific and Technical Information Division. 801 0$bOCLCE 801 1$bOCLCE 801 2$bOCLCQ 801 2$bOCLCO 801 2$bOCLCQ 801 2$bGPO 906 $aBOOK 912 $a9910707804103321 996 $aIntegration effects of D-shaped, underwing, aft-mounted, separate-flow, flow-through nacelles on a high-wing transport$93448935 997 $aUNINA