01562nam 2200445Ka 450 991069809590332120090202083701.0(CKB)5470000002394039(OCoLC)301211106(EXLCZ)99547000000239403920090202d1989 ua 0engtxtrdacontentcrdamediacrrdacarrierStructural and thermal response of 30 cm diameter ion thruster optics[electronic resource] /G.S. MacRae, R.J. Zavesky and S.T. Gooder[Washington, D.C.] :National Aeronautics and Space Administration,[1989]27 pages digital, PDF fileNASA technical memorandum ;102124Title from title screen (viewed Jan. 29, 2009)Finite element methodnasatIon enginesnasatMathematical modelsnasatStructural analysisnasatThermal analysisnasatFinite element method.Ion engines.Mathematical models.Structural analysis.Thermal analysis.MacRae G. S1407468Zavesky R. J1407469Gooder Suzanne T1407470United States.National Aeronautics and Space Administration.GPOGPOBOOK9910698095903321Structural and thermal response of 30 cm diameter ion thruster optics3489076UNINA