NASA Technical Reports Server (NTRS) 19760026195: The 2.5 kW advanced technology ion thruster. design analysis and performance testsReportar como inadecuado




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A representative thruster was extensively documented with respect to performance parameters and characteristics at selected ion beam currents in the 0.5 to 2.75 A range, including measurements of thrust losses resulting from doubly-charged ions and ion beam divergence. Corrected total efficiency was shown to be relatively insensitive to operating p

Autor: NASA Technical Reports Server (NTRS)

Fuente: https://archive.org/







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