CPC B64G 1/58 (2013.01) [B64G 1/546 (2013.01)] | 20 Claims |
1. A spacecraft comprising:
an electronics housing comprising a sun-facing side; and
a peel-and-stick thermal control material coupled to the sun-facing side of the electronics housing, the peel-and-stick thermal control material having an area factor of about 45 ft2/lb and comprising:
a non-metallic optical interface coating having a solar reflectivity for light of wavelength of 250-2500 nm that is greater than or equal to 82% and a solar transmissivity of less than or equal to 2%;
a carrier film; and
an adhesive.
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