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NASA-LLIS-0078

Lessons Learned - Insulation Baking Process for RCS Thrusters

active, Most Current
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.

Document History

NASA-LLIS-0078
May 20, 1992
Lessons Learned - Insulation Baking Process for RCS Thrusters
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...
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