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Validation and Sensitivity Analyses of Arc-Jet Performance of Woven Thermal Protection Entry SystemsA material response model is developed for the determination of erosion rates and thermal response of woven materials to enable accurate thermal protection material sizing and future missions to Venus and giant planets. The stagnation-point thermal response is further evaluated using a Monte Carlo global sensitivity analysis to determine the interactions between key parameters in the material surface energy balance, such as, convective blowing correction parameter and weave material properties including isotropic and orthotropic thermal conductivites. The time-accurate material response for the dual layer weave erosion and surface temperatures show excellent agreement with stagnation flat face arc-jet tests involving time-varying aeroheating-cooling cycles. The high-fidelity Monte Carlo sensitivity analysis technique was used to address challenges in thermal protection sizing for the Adaptive Deployable Entry and Placement Technology (ADEPT) system, a low ballistic coefficient hypersonic decelerator. The results represent new correlations for such weaves involving Carbon-air oxidation equilibrium chemistry. Through the multi-variate regression analyses and uncertainty rankings performed, only three properties were found to contribute to the transient thermal response of the gore, with emissivity contributing to nearly 95% of the total output uncertainty.
Document ID
20210017979
Acquisition Source
Ames Research Center
Document Type
Conference Paper
Authors
Pratibha Raghunandan
(Analytical Mechanics Associates (United States) Hampton, Virginia, United States)
Eric Stern
(Ames Research Center Mountain View, California, United States)
Justin Haskins
(Ames Research Center Mountain View, California, United States)
Date Acquired
June 27, 2021
Subject Category
Spacecraft Design, Testing And Performance
Meeting Information
Meeting: AIAA AVIATION Forum and Exposition
Location: Virtual
Country: US
Start Date: August 2, 2021
End Date: August 6, 2021
Sponsors: American Institute of Aeronautics and Astronautics
Funding Number(s)
CONTRACT_GRANT: NNA15BB15C
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
NASA Technical Management
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