Fluid-loop reaction system

Aeronautics and astronautics – Spacecraft – Attitude control

Patent

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Details

244165, 114122, 114125, B64G 128

Patent

active

050260081

ABSTRACT:
An improved fluid actuating system for imparting motion to a body such as a spacecraft is disclosed. The fluid actuating system consists of a fluid mass that may be controllably accelerated through at least one fluid path whereby an opposite acceleration is experienced by the spacecraft. For full control of the spacecraft's orientation, the system would include a plurality of fluid paths. The fluid paths may be circular or irregular, and the fluid paths may located on the interior or exterior of the spacecraft.

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