LEADER 01562nam  2200445Ka 450 
001 9910698095903321
005 20090202083701.0
035   $a(CKB)5470000002394039
035   $a(OCoLC)301211106
035   $a(EXLCZ)995470000002394039
100   $a20090202d1989      ua             0
101 0 $aeng
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aStructural and thermal response of 30 cm diameter ion thruster optics$b[electronic resource] /$fG.S. MacRae, R.J. Zavesky and S.T. Gooder
210  1$a[Washington, D.C.] :$cNational Aeronautics and Space Administration,$d[1989]
215   $a27 pages $cdigital, PDF file
225 1 $aNASA technical memorandum ;$v102124
300   $aTitle from title screen (viewed Jan. 29, 2009)
606   $aFinite element method$2nasat
606   $aIon engines$2nasat
606   $aMathematical models$2nasat
606   $aStructural analysis$2nasat
606   $aThermal analysis$2nasat
615  7$aFinite element method.
615  7$aIon engines.
615  7$aMathematical models.
615  7$aStructural analysis.
615  7$aThermal analysis.
700   $aMacRae$b G. S$01407468
701   $aZavesky$b R. J$01407469
701   $aGooder$b Suzanne T$01407470
712 02$aUnited States.$bNational Aeronautics and Space Administration.
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910698095903321
996   $aStructural and thermal response of 30 cm diameter ion thruster optics$93489076
997   $aUNINA