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
Link To Document :
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