Foil deployment mechanism
AssigneeEuropean Space Agency
InventorPaul HODGETTS
Life of this patent
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AssigneeEuropean Space Agency
InventorPaul HODGETTS
Estimating the term…
A foil deployment mechanism comprises a first drum rotatable about a first longitudinal axis, and a second drum rotatable about a second longitudinal axis. The foil deployment mechanism further comprises a cable, the cable comprising a first section which extends from a lower part of the second drum to an upper part of the first drum, a second section which is wound around a part of the first drum facing away from the second drum, a third section which extends from a lower part of the first drum to an upper part of the second drum, and a fourth section which is wound around a part of the second drum facing away from the first drum, wherein the first section and the third section intersect each other between the first drum and the second drum when being viewed along the first longitudinal axis.
1-16. (canceled)
A foil deployment mechanism, comprising:
A foil deployment system,
Dependencies are inferred from the claim text.