Aeronautics and astronautics – Spacecraft – Attitude control
Patent
1989-02-22
1991-08-20
Barefoot, Galen
Aeronautics and astronautics
Spacecraft
Attitude control
B64G 162
Patent
active
050407490
ABSTRACT:
A spacecraft berthing mechanism comprises a peripheral flange adapted for attachment to a spacecraft port, an impact receiving member pivotably attached to the peripheral flange, and a motion damping device connected between the impact receiving device and the peripheral flange. Edge-on berthing between two such berthing mechanisms allows for placement of the impact receiving members and damping devices along only a minor portion of the circumference of the berthing interface, thereby minimizing both the weight and complexity of the structure. The motion damping devices are of the non-rebound type and reset automatically after absorbing berthing impacts.
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Barefoot Galen
Ellis Christopher P.
Space Industries, Inc.
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