Numerous charts are presented showing values of the various parameters involved in space-vehicle electricpower systems. Characteristics are given of solar batteries, fuel cells, thermoelectric cells, thermionic cells, gas turbine engines, turbines, storage batteries, and reciprocating englnes. Aithough primarily concerned with electric power components, generation and energy conversion are also discussed with respect to load and energy storage. (N.W.R.)

ELECTRIC POWER FOR SPACE VEHICLES

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