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Vacuum/Zero Net-Gravity Application for On-Orbit TPS Tile RepairThe Orbiter Columbia catastrophically failed during reentry February 1, 2003. All space Shuttle flights were suspended, including logistics support for the International Space Station. NASA LaRC s Structures and Materials Competency is performing characterizations of candidate materials for on-orbit repair of orbiter Thermal Protection System (TPS) tiles to support Return-to-Flight activities led by JSC. At least ten materials properties or attributes (adhesion to damage site, thermal protection, char/ash strength, thermal expansion, blistering, flaming, mixing ease, application in vacuum and zero gravity, cure time, shelf or storage life, and short-term outgassing and foaming) of candidate materials are of interest for on-orbit repair. This paper reports application in vacuum and zero net-gravity (for viscous flow repair materials). A description of the test apparatus and preliminary results of several candidate materials are presented. The filling of damage cavities is different for some candidate repair materials in combined vacuum and zero net-gravity than in either vacuum or zero net- gravity alone.
Document ID
20040167158
Acquisition Source
Langley Research Center
Document Type
Preprint (Draft being sent to journal)
Authors
Harvey, Gale A.
(NASA Langley Research Center Hampton, VA, United States)
Humes, Donald H.
(NASA Langley Research Center Hampton, VA, United States)
Siochi, Emilie J.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2004
Subject Category
Spacecraft Design, Testing And Performance
Meeting Information
Meeting: 23rd Space Simulation Conference
Location: Annapolis, MD
Country: United States
Start Date: November 8, 2004
End Date: November 11, 2004
Funding Number(s)
OTHER: 376-70-30-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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