Method and apparatus for satellite orbital change using...

Aeronautics and astronautics – Spacecraft – Tethered

Reexamination Certificate

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C244S158600, C244S172500, C244S172600

Reexamination Certificate

active

08052092

ABSTRACT:
An apparatus for orbital change of a satellite incorporates a capture mechanism for space debris and a tether connecting the capture mechanism to a satellite. The tether is extendable to position the capture mechanism relative to the space debris. A controller is employed for timed release of the space debris by the capture mechanism for orbital change by the satellite.

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