Deployment sequencer

Aeronautics and astronautics – Spacecraft – With payload accommodation

Patent

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Details

136245, 136246, B64G 144

Patent

active

059098600

ABSTRACT:
In order to control the deployment of secondary deployment structures in a deployment system that includes both a primary and a secondary deployment, an improved deployment sequencer utilizes the rotational motion of primary deployment structures. In particular, the rotational motion serves to control the retention and release of the secondary deployment structures during the primary deployment. Still more specifically, the deployment sequencer restrains the deployment of the secondary deployment structures until the primary deployment structures have deployed or rotated far enough so that collisions between the secondary deployment structures are avoided.

REFERENCES:
patent: 5393018 (1995-02-01), Roth et al.
patent: 5520747 (1996-05-01), Marks
patent: 5785280 (1998-07-01), Baghdasarian
patent: 5810296 (1998-09-01), Izumi

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