NASA NTRS · 19710045532
Application of parameter optimization techniques to space shuttle thermal protection design
Abstract
Space shuttle thermal protection system optimal weight by numerical parameterization, discussing temperature constraints and material rearrangement effects
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Curry, D. M., Williams, S. D.. 1971-04-01. Application of parameter optimization techniques to space shuttle thermal protection design. https://ntrs.nasa.gov/citations/19710045532
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