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Development of CST(registered) for a Solventless Sprayable Coating, MCC-1This paper discusses an innovative process called convergent spray technology (CST), as applied to the development and successful implementation of MCC-1 coating for the Shuttle/SRB as a primary Thermal Protection System (TPS). The session will illustrate the environmental and the process benefits of the MCC-1 technology, show the systematic steps taken for the development of the technology that included statistically conducted sensitivity studies of about 34 variables, and illustrate that the technology is "Field-proven" based on the process and post-flight successes on the Shuttle/SRB. The application of this technology to other aerospace and commercial programs will be introduced to illustrate the wide range of possibilities.
Document ID
19990084049
Acquisition Source
Marshall Space Flight Center
Document Type
Abstract
Authors
Patel, A. K.
(NASA Marshall Space Flight Center Huntsville, AL United States)
Meeks, C.
(NASA Marshall Space Flight Center Huntsville, AL United States)
Date Acquired
August 19, 2013
Publication Date
January 1, 1998
Subject Category
Nonmetallic Materials
Meeting Information
Meeting: Technology 2008
Location: Boston, MA
Country: United States
Start Date: November 3, 1998
End Date: November 5, 1998
Funding Number(s)
CONTRACT_GRANT: NAS8-36300
Distribution Limits
Public
Copyright
Other

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