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- W2128858015 abstract "In aerospace instruments, the problem of temperature control can become severe because convettive cooling cannot be used; heat must be transferred by radiative means alone. Systems are exposed to a rigorous thermal environment and there are strict limitations on the power, weight and volumes available. A surprisingly high degree of temperature control can be accomplished, however, by the use of a passive system of spectrally selective surfaces. In this paper, one approach to the design of passive temperature control systems is discussed by detailed reference to an instrument intended for use on the lunar surface." @default.
- W2128858015 created "2016-06-24" @default.
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- W2128858015 date "1966-06-01" @default.
- W2128858015 modified "2023-09-27" @default.
- W2128858015 title "Passive Temperature Control System for An Aerospace Instrument" @default.
- W2128858015 doi "https://doi.org/10.1243/pime_proc_1966_181_032_02" @default.
- W2128858015 hasPublicationYear "1966" @default.
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