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

Prabhu, Dinesh K

关键词: ATMOSPHERIC ENTRY;    BALLISTIC TRAJECTORIES;    CARBON-PHENOLIC COMPOSITES;    CONVECTIVE HEAT TRANSFER;    FLIGHT PATHS;    HEAT FLUX;    HEAT SHIELDING;    NOSE CONES;    PLANETARY ATMOSPHERES;    SPACECRAFT SHIELDING;    THERMAL PROTECTION;   

RP-ID  :  ARC-E-DAA-TN60768

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来源: NASA Technical Reports Server

【 摘 要 】

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