4. Basic Selection Criteria of Heat-Resistant and Thermal Protective Structures for High-Altitude Hypersonic Flying Vehicle

4. Basic Selection Criteria of Heat-Resistant and Thermal Protective Structures for High-Altitude Hypersonic Flying Vehicle

Gusarova I. А., Potapov А. М., Golubkov G. М., Kalinichenko D. S., Poluyan N. V., Man’ko Т. А.

Yangel Yuzhnoye State Design Office, Dnipro, Ukraine

Oles Honchar Dnipro National University, Dnipro, Ukraine

Kosm. teh. Raket. vooruž. 2017 (1); 23-29
 
Language: Russian
Annotation:
The thermal analysis was made for external surfaces of a reusable high-altitude supersonic flying vehicle being a part of a space transportation system. The basic criteria were determined for selection of its heat-resistant and heat-protective structures.

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