Gyrodynamic fixture for measuring thrust force components

Radiant energy – Photocells; circuits and apparatus – Optical or pre-photocell system

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73116, 356154, G01D 534

Patent

active

042141567

ABSTRACT:
Apparatus for measuring rocket motor thrust components and resolving small ector alignment errors. Apparatus includes a spherical air bearing which embodies gyrodynamic principles in order to provide three degrees of angular freedom and in order to achieve stiff, vibration free reactions against translational movement. Effects of thrust misalignment are seen as changes in angular rate which can be measured by encoding rotations of the floated rocket motor inner bearing assembly by use of built-in sensors and/or by motion with an external optical tracker.

REFERENCES:
patent: 3137531 (1964-06-01), Herrmann et al.

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