NASA NTRS · 19720019034
Study of solid rocket motor for a space shuttle booster. Appendix B: Typical component recertification test procedures
Abstract
Flexseal assemblies, TVC actuators, hydraulic supply system, TVC electronic control unit, flight instrumentation system, ordnance system electronics, and hydrotest of SRM case segments are discussed, applied to typical component recertification test procedures.
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1972-03-15. Study of solid rocket motor for a space shuttle booster. Appendix B: Typical component recertification test procedures. https://ntrs.nasa.gov/citations/19720019034
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