Space object deployment system and method

Aeronautics and astronautics – Spacecraft – With payload accommodation

Reexamination Certificate

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Details

C244S164000

Reexamination Certificate

active

07967257

ABSTRACT:
Provided is a space object deployment system. Specifically, the system in at least one embodiment, includes at least one deployable object. A deployment chamber is paired with each deployable object, each chamber including: a base opposite from the deployable object; and a spring loaded countermass coupled to the base and slidably disposed within the chamber, the deployment chamber at least partially disposed within a rotatable body transverse to the axis of rotation. At least one coupler is paired to each deployable object and adapted to detachably couple the deployable object to the body and constrain the countermass within the chamber. An associated method of use is provided as well.

REFERENCES:
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patent: 4181062 (1980-01-01), Bernstein et al.
patent: 4506852 (1985-03-01), Adams et al.
patent: 6126115 (2000-10-01), Carrier et al.
patent: 7373886 (2008-05-01), Zatterqvist et al.

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