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Verification of RSRM Nozzle Thermal Models With ETM-3 Aft Exit Cone In-depth Temperature MeasurementsOne of the goals of the Engineering Test Motor (ETM-3) static test was to verify analytical models through the use of instrumentation that provide real-time transient temperature response of ablating phenolic liners. Accurate measurement of in-depth temperature is critical for validating the analytical models and assessing design safety margins for nozzle insulation materials. Recent developments of in-depth thermocouple plugs have been made to more accurately measure temperature response of nozzle Liners. Thermocouple plugs were installed at two axial stations (four plugs circumferentially at each station) near the end of the ETM-3 nozzle aft exit cone to gather temperature histories during and after motor operation. The thermocouple plugs were placed at depths that bounded the reusable solid rocket motor nominal measured char depth in order to portray the carbon phenolic temperature response during the charring process. The data were used to verify the analytical models during motor operation and to better define char penetration during heat soak after motor burn out.
Document ID
20040085893
Acquisition Source
Marshall Space Flight Center
Document Type
Preprint (Draft being sent to journal)
Authors
Maw, Joel F.
(ATK-Thiokol Propulsion Brigham City, UT, United States)
Lui, Robbie C.
(ATK-Thiokol Propulsion Brigham City, UT, United States)
Totman, Peter D.
(ATK-Thiokol Propulsion Brigham City, UT, United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2004
Publication Information
Publisher: American Inst. of Aeronautics and Astronautics
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
AIAA Paper 2004-3897
Report Number: AIAA Paper 2004-3897
Meeting Information
Meeting: 40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
Location: Fort Lauderdale, FL
Country: United States
Start Date: July 11, 2004
End Date: July 14, 2004
Sponsors: American Society for Electrical Engineers, American Inst. of Aeronautics and Astronautics, American Society of Mechanical Engineers, Society of Automotive Engineers, Inc.
Funding Number(s)
CONTRACT_GRANT: NAS8-97238
Distribution Limits
Public
Copyright
Public Use Permitted.
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