NASA NTRS · 19710019981
Ablative leading edge design concepts for the shuttle orbiter
Abstract
Design of low cost ablator leading edge for space shuttle thermal protection system
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Graham, J. W., Mosher, D. A., Victer, I.. 1971-04-01. Ablative leading edge design concepts for the shuttle orbiter. https://ntrs.nasa.gov/citations/19710019981
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