The incorporation of nickel-hydrogen technology into spacecraft power system designs for low Earth orbit vehicles offers significant power system weight reductions by increasing the power storage watt-hour efficiency. Several possible module configurations exist for the power system. The module configurations were compared utilizing reliability, weight, volume and load capability as evaluation parameters.
Nickel-hydrogen spacecraft module configurations study
1985-07-01
Aufsatz (Konferenz)
Keine Angabe
Englisch
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