DocumentCode
1227192
Title
Multi-Component Test Fixtures for Solid Rocket Motor Testing
Author
Langill, A.W. ; Kapandritis, G.N.
Author_Institution
Aerojet-General Corporation Sacramento, California
Volume
1
Issue
2
fYear
1963
Firstpage
86
Lastpage
98
Abstract
In the static testing of large solid rocket motors, particularly those equipped with a form of steering system, a multiple degree-of-freedom test fixture is normally employed. This paper discusses multi-component test fixtures within a basic conceptual framework. A qualitative description of the specific form of mechanical system used is given. The choice of force cell measurement devices and associated isolators used with multi-component test fixtures is described. Conventional static and dynamic systems calibrations to support accuracy considerations are determined. A discussion of the dynamic considerations in multi-component test data analysis and reduction processes including digital data compensation techniques for improving the quality of force information, derived from the multi-component test fixture environment, are suggested.
Keywords
Calibration; Data analysis; Fixtures; Force measurement; Isolators; Mechanical systems; Rockets; Solids; Steering systems; System testing;
fLanguage
English
Journal_Title
Aerospace, IEEE Transactions on
Publisher
ieee
ISSN
0536-1516
Type
jour
DOI
10.1109/TA.1963.4319369
Filename
4319369
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