Spacecraft Heat Shield
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United States of America Patent
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Issued Date -
Aug 15, 2024
app pub date -
Aug 30, 2022
filing date -
Aug 27, 2021
priority date (Note) -
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status (Latency Note)
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Abstract
Spacecraft Heat Shield A deployable spacecraft atmospheric-entry heat shield (30, 40, 50, 60) is configured in a flasher pattern with a transformable polyhedral-surface. The transformable polyhedral-surface has a plurality of sectors (2, see FIG. 1a), each sector (2) having a plurality of mountain fold lines (4, 5), a plurality of valley fold lines (6, 7), a plurality of facets (8) lying between the fold lines (4, 5, 6, 7) and an outside edge (12). The heat shield (30, 40, 50, 60) is configured to unfold from a stowed configuration to a deployed configuration.
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