NASA-LLIS-0078
Lessons Learned - Insulation Baking Process for RCS Thrusters
| Organization: | NASA |
| Publication Date: | 20 May 1992 |
| Status: | active |
| Page Count: | 2 |
scope:
Description of Driving Event:
Three RCS primary thruster injector/chamber assemblies were damaged when the oven temperature control system malfunctioned and permitted the temperature to reach an estimated 1400 deg F during a cerachrome insulation baking process that should have been limited to 625 deg F. These units should have been rejected at this point, but quality assurance was not notified. As a result, the full extent of damage was not determined until the severe discoloration of titanium alloy and columbium parts was noted during the post-baking weighing process, about three weeks later.
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