FIELD: astronautics.
SUBSTANCE: invention relates to the spacecrafts (SC) power equipment. Installation contains the nuclear reactor, radiation protection, a refrigerator-emitter and the deployment system (in the form of a rod frame) from the folded state into the working state. Installation is equipped with at least one thermionic electrons source, radiating in the nuclear reactor direction, and at least one pair of coaxial and oppositely directed nozzles, attached to the cylinder with compressed gas. One of the nozzles is directed towards the nuclear reactor. Electrons source accelerates the gas ions recombination, “blown off” from the nuclear reactor by the nozzle.
EFFECT: technical result consists in reduction in the SC gas-dust environment charged particles influence on its onboard equipment operation.
3 cl, 1 dwg
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Authors
Dates
2019-01-16—Published
2017-12-27—Filed