A multilayer particle shield for a spacecraft includes an inboard exterior layer configured to be disposed proximal to the spacecraft, an outboard exterior layer configured to be disposed distal from the spacecraft and at least one interior layer disposed between the inboard exterior layer and the outboard exterior layer, wherein the interior layer includes a semi-rigid, porous, compressible spacer.
Flexible micrometeoroid shield
14.06.2022
Patent
Elektronische Ressource
Englisch
Europäisches Patentamt | 2022
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