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NASA-LLIS-0177

Lessons Learned - Solid Rocket Motor (SRM) O-ring

active, Most Current
Organization: NASA
Publication Date: 23 October 1992
Status: active
Page Count: 2
scope:

Description of Driving Event:

The o-ring used in the SRM case joint is critical to the sealing of the joint, yet is not designated as a critical process. The adequacy of o-ring processing and quality control is questionable even though a number of o-rings in bonded storage were thoroughly analyzed and tested as part of 51-L failure analysis effort and found to be acceptable. The manufacturing process included delivery of the final o-ring rubber material to where the material is cut to the proper lengths and a scarf joint is made. This manufacturing process is a potential problem area as seen by repairs of inclusions and voids in the rubber delivered.

Document History

NASA-LLIS-0177
October 23, 1992
Lessons Learned - Solid Rocket Motor (SRM) O-ring
Description of Driving Event: The o-ring used in the SRM case joint is critical to the sealing of the joint, yet is not designated as a critical process. The adequacy of o-ring processing and...
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