The usual way to provide energy for space vehicles is to use solar photovoltaic panels, or produce electric energy from fuel cells [AtE Jul 77], i.e., from chemically stored energy in fuels taken along from the earth. The main constraint is weight per power, which is now from 6 to 10 kg per kW, including regulation, control and battery-charging electronics; but NASA would like to reduce the ratio to 5 kg/kW by the end of the decade, and to 1 kg/kW by the end of the century. This constraint pretty well rules out nuclear power; the lead shielding makes reactors too heavy.
One proposal under consideration for powering a number of space vehicles is to have a central, stationary space power satellite that would collect solar energy and beam it to other spacecraft.
The sunlight could be turned into electricity either via photoelectric cells, or even thermally
¾using that part of the steam (or other gas) that is not needed for the process heat used for some other purpose on the spot. The electric power would then be used to beam the energy via electromagnetic radiation (radiowaves or light) to the recipient spacecraft.An alternative is to use the incident sunlight to power the "pump" of a laser. The pump is a device using high-intensity incoherent (i.e., regular) light to stimulate the atoms in a gas, which then emit coherent laser light, a very pure, penetrating, powerful type of light that could carry the energy in thin, precisely controllable beams.
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Vol. 8, No. 10
Newsletter: Access to Energy Newsletter Archive Volume: Issues Issue/No.: Vol. 8, No. 10 Date: November 23, 2004 11:51 AM (For actual publication date see newsletter.) Title: Defending the environment against the Sierra Club
Copyright © 2004 - Access to Energy Newsletter Archive
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