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Development of a Enhanced Thermal Barrier for RSRM Nozzle JointsA carbon fiber rope is being considered as replacement for the RTV thermal barrier that is currently used to protect o-rings in RSRM nozzle joints, Performance requirements include its ability to cool propellant gases filter slag and particulates, and conform to various joint assembly conditions as well as dynamic flight motion. Testing has shown its superior heat resistance, even in oxidative and corrosive environments. Testing has also demonstrated excellent performance of this system in sub-scale motors. Cold flow testing, has demonstrated its ability to conform to motor dynamics. Manufacture and assembly testing have demonstrated the ease of gland machining as well as assembly in a full-scale nozzle.
Document ID
20000092509
Acquisition Source
Marshall Space Flight Center
Document Type
Preprint (Draft being sent to journal)
Authors
Bauer, P. H.
(Thiokol Propulsion Brigham City, UT United States)
McCool, A.
Date Acquired
August 19, 2013
Publication Date
January 1, 2000
Publication Information
Publisher: American Inst. of Aeronautics and Astronautics
Subject Category
Spacecraft Propulsion And Power
Meeting Information
Meeting: Joint Propulsion
Location: Huntsville, AL
Country: United States
Start Date: July 16, 2000
End Date: July 19, 2000
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
CONTRACT_GRANT: NAS8-38100
Distribution Limits
Public
Copyright
Other

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