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Characterization of Internal Insulation Thermal PerformanceA test campaign was performed to build an SRM-insulation-material thermal-performance database using MSFC’s Solid Fuel Torch that could be leveraged to enhance understanding of the relationship between ablation rates and internal-environment parameters and improve insulation performance predictions. Seven hot-fire tests were performed along with data analysis that revealed the thermal performance differences among the tested materials. Functional Data Analysis was employed to create a model of material ablation rate as a function of six covariates. The relative importance of several environmental parameters was indicated, and the gaps in the operational space covered by the database were identified.
Document ID
20240009657
Acquisition Source
Langley Research Center
Document Type
Technical Memorandum (TM)
Authors
Jonathan E. Jones
(Langley Research Center Hampton, United States)
Heath T. Martin
(Marshall Space Flight Center Redstone Arsenal, United States)
James M. Womack
(Northern Nevada Statistical Consulting)
Andrew T. Hiatt
(Marshall Space Flight Center Redstone Arsenal, United States)
Date Acquired
July 29, 2024
Publication Date
July 1, 2024
Subject Category
Fluid Mechanics and Thermodynamics
Report/Patent Number
NESC-RP-19-01482
Funding Number(s)
WBS: 869021.01.23.01.01
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
NASA Peer Committee
Keywords
Ablation
Insulation;
Solid Rocket Motor
Hybrid Rocket Motor
Functional Data Analysis
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