The reusable Manned Space Shuttle has been flying into Space and returning to earth for more than 25 years. The launch pad environment can be corrosive to metallic substrates and the Space Shuttles are exposed to this environment when preparing for launch. The Orbiter has been in service well past its design life of 10 years or 100 missions. As part of the aging vehicle assessment one question under evaluation is how the thermal protection system and aging protective coatings are performing to insure structural integrity. The assessment of this cost resources and time. The information is invaluable when minimizing risk to the safety of Astronauts and Vehicle. This paper will outline a strategic sampling plan and some operational improvements made by the Orbiter Structures team and Corrosion Control Review Board.
Space Shuttle Corrosion Protection Performance
10th DoD/NASA/FAA Aging Aircraft Conference ; 2007 ; Palm Springs, CA, United States
2007-04-16
Conference paper
No indication
English
Space Shuttle Lightning Protection
NTRS | 1979
|Lightning Protection System for Space Shuttle
NTIS | 1977
Lightning Protection System for Space Shuttle
NTRS | 1977
Shuttle Space Suit Glove Thermal Protection and Performance Improvement Evolution
SAE Technical Papers | 1994
|