REG NASA-LLIS-0176-1992 Lessons Learned - Solid Rocket Motor (SRM) Field Joints and Configuration.pdf
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1、Lessons Learned Entry: 0176Lesson Info:a71 Lesson Number: 0176a71 Lesson Date: 1992-10-23a71 Submitting Organization: KSCa71 Submitted by: Lisa L. MusgraveSubject: Solid Rocket Motor (SRM) Field Joints and Configuration Description of Driving Event: The primary reason for the use of the putty in the
2、 SRM was to act as a thermal barrier in the joints to prevent o-ring erosion resulting from circumferential hot gas flow during motor firing. Prior to the 51-L mishap, the putty was believed to perform such that it would allow pressure to the primary o-ring during the SRM ignition transient. Subsequ
3、ently, it has been found that humidity and temperature enhance the characteristics of putty relative to its pressure holding characteristics. The uncertainty of these characteristic changes directly affected the ability of the field joint to seal.Lesson(s) Learned: 1. Insufficient knowledge of perfo
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