• 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