Satellite air brake wing structure

A deployable wing structure for air-braking a satellite and which, once deployed, includes at least one wing structure element that forms a three-dimensional structure and includes at least two panels lying in secant planes and forming a dihedron.

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Bibliographische Detailangaben
Hauptverfasser: Peypoudat, Vincent, Le Couls, Olivier
Format: Patent
Sprache:eng
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Beschreibung
Zusammenfassung:A deployable wing structure for air-braking a satellite and which, once deployed, includes at least one wing structure element that forms a three-dimensional structure and includes at least two panels lying in secant planes and forming a dihedron.