FIELD: transport.
SUBSTANCE: invention relates to space engineering, namely to thermal protection of spacecraft. Spacecraft thermal blanket with outer combined coat consists of polymer base, electrically conducting layer with wear-resistant layer on outer surface and reflecting layer on inner surface. Proposed thermal blanket comprises temporary protective layer on outer surface and reinforcing polymer screen on inner surface.
EFFECT: higher reliability and efficiency, reduced weight and dust-and-frieze emission.
5 cl, 4 tbl, 2 dwg
| Title | Year | Author | Number |
|---|---|---|---|
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|
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