Spacecraft berthing mechanism

Aeronautics and astronautics – Spacecraft – Attitude control

Patent

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Details

244158R, B64G 164, B64G 122

Patent

active

053988922

ABSTRACT:
A spacecraft berthing mechanism for coupling spacecraft is provided which has minimal effect on the maximum size an associated spacecraft hull may have. The berthing mechanism includes a flange member which defines a hatchway and which is adapted for attachment to a spacecraft port. The flange member has a forwardly facing interface surface through which the hatchway passes and an outer peripheral surface extending rearwardly from the interface surface. The peripheral surface has a plurality of beveled portions spaced substantially evenly about the peripheral surface. A plurality of alignment guides are arranged on the flange member such that several of the alignment guides are positioned adjacent one of the beveled portions and the remaining alignment guides are positioned adjacent an opposing beveled portion.

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