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In view of the problem that the design of traditional thermal protection system is not suitable for the extreme force and thermal environment during the long endurance and high Mach flight of supersonic/hypersonic vehicle, the concept of a combined thermal protection system is put forward, and the research of combined thermal protection system is introduced from the aspects of protection/heat insulation performance and load-bearing performance. The performance and research status are summarized emphatically for the filling-combined thermal protection system. By comparing the characteristics of the combined thermal protection system, it is found that the structural efficiency of the filling-combined system is higher, but the processing technology is more complex. The thermal insulation capacity of the combined thermal structure is limited by the thickness of the thermal insulation material. The combined thermal protection system is more efficient with new high-temperature resistant materials or high-temperature heat pipes. It is the key to solve the lightweight design of the structure. The development trend is prospected for the lightweight thermal protection system design of supersonic/hypersonic vehicle.
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Basic Information:
DOI：10.16358/j.issn.1009-1300.20220142
China Classification Code:V244.1;V445.1
Citation Information:
[1]Li Shibin,Ma Rui,Wang Lin.A review of combined thermal protection system for high-speed aircraft[J].Tactical Missile Technology,2023,No.217(01):8-21.DOI:10.16358/j.issn.1009-1300.20220142.
Fund Information:
国家自然科学基金（11802340）
2023-01-15
2023-01-15