Spacecraft with deployable panel array
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United States of America Patent
Stats
-
Nov 12, 2002
Grant Date -
Jun 20, 2002
app pub date -
Nov 2, 1998
filing date -
Nov 2, 1998
priority date (Note) -
In Force
status (Latency Note)
Importance
Abstract
A spacecraft, such as a satellite, comprises a panel array including a plurality of panels that are rotatably coupled to one another. The panel array is movable between a folded state and an extended state. In the folded state, the panels are stacked atop one another. In the extended state, the panels are positioned such that active surfaces of the panels are aligned within a common plane. A plurality of hinge mechanisms preferably rotatably couple the panels to one another. The hinge mechanisms are configured to move the panel array from the folded state to the extended state without interfering with the active surfaces of the panels when the panel array is extended.
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