LEADER 02290nam 2200709Ia 450 001 9910700284303321 005 20110323135837.0 035 $a(CKB)5470000002408130 035 $a(OCoLC)708253122 035 $a(EXLCZ)995470000002408130 100 $a20110323d1984 ua 0 101 0 $aeng 135 $aurbn||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aAdvanced ion thruster research$b[electronic resource] /$fPaul J. Wilbur ; prepared for Lewis Research Center, National Aeronautics and Space Administration 210 1$aFort Collins, CO :$cColorado State University, Department of Mechanical Engineering ;$a[Springfield, Va.]:$c[For sale by the National Technical Information Service],$d[1985] 215 $a1 online resource (iv, 58 pages) 225 1 $aNASA CR ;$v174862 300 $aTitle from title screen (viewed Mar. 22, 2011). 300 $a"Jan. 1985." 320 $aIncludes bibliographical references (pages 57-58) 606 $aAnodes$2nasat 606 $aCathodes$2nasat 606 $aDeflection$2nasat 606 $aDivergence$2nasat 606 $aElectric potential$2nasat 606 $aGas pressure$2nasat 606 $aHollow cathodes$2nasat 606 $aIon beams$2nasat 606 $aIon engines$2nasat 606 $aIon propulsion$2nasat 606 $aIon sheaths$2nasat 606 $aMagnetic fields$2nasat 606 $aNitrogen$2nasat 606 $aRing discharge$2nasat 606 $aXenon$2nasat 615 7$aAnodes. 615 7$aCathodes. 615 7$aDeflection. 615 7$aDivergence. 615 7$aElectric potential. 615 7$aGas pressure. 615 7$aHollow cathodes. 615 7$aIon beams. 615 7$aIon engines. 615 7$aIon propulsion. 615 7$aIon sheaths. 615 7$aMagnetic fields. 615 7$aNitrogen. 615 7$aRing discharge. 615 7$aXenon. 700 $aWilbur$b Paul J$01390997 712 02$aLewis Research Center. 712 02$aColorado State University.$bDepartment of Mechanical Engineering. 801 0$bGPO 801 1$bGPO 906 $aBOOK 912 $a9910700284303321 996 $aAdvanced ion thruster research$93463392 997 $aUNINA LEADER 02268nam 2200541Ia 450 001 9910700302703321 005 20110628101248.0 035 $a(CKB)5470000002409965 035 $a(OCoLC)733290865 035 $a(EXLCZ)995470000002409965 100 $a20110628d2010 ua 0 101 0 $aeng 135 $aurcn||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aACT payload shroud structural concept analysis and optimization$b[electronic resource] /$fBart F. Zalewski, Brett A. Bednarcyk ; prepared for the 16th U.S. National Congress on Theoretical and Applied Mechanics (USNCTAM) sponsored by the U.S. Committee on Theoretical and Applied Mechanics, University Park, Pennsylvania, June 27-July 2, 2010 210 1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$d[2010] 215 $a1 online resource (14 pages) $ccolor illustrations 225 1 $aNASA/TM ;$v2010-216942 300 $aTitle from title screen (viewed on June 27, 2011). 300 $a"December 2010." 320 $aIncludes bibliographical references (page 14) 517 3 $aAdvanced Composites Technology payload shroud structural concept analysis and optimization 606 $aStructural design$2nasat 606 $aFiber composites$2nasat 606 $aFinite element method$2nasat 606 $aLaunch vehicles$2nasat 606 $aComposite structures$2nasat 606 $aStructural analysis$2nasat 606 $aAres 5 cargo launch vehicle$2nasat 615 7$aStructural design. 615 7$aFiber composites. 615 7$aFinite element method. 615 7$aLaunch vehicles. 615 7$aComposite structures. 615 7$aStructural analysis. 615 7$aAres 5 cargo launch vehicle. 700 $aZalewski$b Bartlomiej Francisze$01390011 701 $aBednarcyk$b Brett A$01389323 712 02$aNASA Glenn Research Center. 712 12$aU.S. National Congress of Theoretical and Applied Mechanics$d(16th :$f2010 :$eUniversity Park, Pa.) 801 0$bGPO 801 1$bGPO 906 $aBOOK 912 $a9910700302703321 996 $aACT payload shroud structural concept analysis and optimization$93458300 997 $aUNINA