Liquid balance control for spinning spacecraft

Aeronautics and astronautics – Spacecraft – Attitude control

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Details

244165, 244135C, 244 93, B64G 124

Patent

active

050588346

ABSTRACT:
The balance of a spin-balanced spacecraft may be dynamically adjusted by moving a liquid between or among containers spaced about the spin axis. The transfer of liquid is accomplished by controllable heaters associated with each container, for heating that container from which liquid is to be transferred to increase the pressure and drive out liquid. A spacecraft for accomplishing this method includes a balance sensing arrangements such as a gyroscope and logic for determining which container or containers are to be emptied and for controlling the heaters. Weight is minimized by accomplishing the transfer of liquid among fuel containers by way of manifolds which also supply fuel to thrusters.

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Lorell et al., "An Automatic Mass-Trim Sys. for Spinning Spacecraft".
"The Stabilization System" by Goel et al., published at pp. 135-143 of the Proceedings of the Indian Academy of Science, vol. C1, No. 2, Sep. 1978.

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