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oaioai:casi.ntrs.nasa.gov:20190002181

Exploration of the Viability of HEEET as a TPS for Saturn, Neptune, and Uranus Entries

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2018
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Abstract

Exploration of ballistic coefficient and entry flight path angle to determine loom requirements for weaving a dual-layer thermal protection material such as HEEE

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This paper was published in NASA Technical Reports Server.

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