Life Evaluation of Thermal Protective Coatings for Air-launched Missiles

ZHANG Kai, YANG Mingjia, YANG Xiaokui, SHI Haobo

Equipment Environmental Engineering ›› 2026, Vol. 23 ›› Issue (1) : 17-24.

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Equipment Environmental Engineering ›› 2026, Vol. 23 ›› Issue (1) : 17-24. DOI: 10.7643/ issn.1672-9242.2026.01.003
Weapons Equipment

Life Evaluation of Thermal Protective Coatings for Air-launched Missiles

  • ZHANG Kai1, YANG Mingjia2, YANG Xiaokui1*, SHI Haobo2
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Abstract

The work aims to establish a test and life evaluation method for thermal protective coatings of air-launched missiles that closely resembles the profile of the service environment. Firstly, based on the analysis results of the environmental profile throughout the missiles' life cycle, and considering the two main environments of depot storage and on-duty ferry flight, the accelerated test profile and test load spectrum were constructed by comprehensively considering simulation and acceleration. Then, on this basis, in accordance with the principle of equivalent environmental effects, the acceleration factor was determined by drawing on the temperature and humidity coupling model for analysis. Finally, based on the performance test results of the thermal protective coatings after the equivalent expected life accelerated test, the service life of the coatings was evaluated with the failure threshold as the criterion.An accelerated test method for thermal protective coatings involving environmental factors such as temperature, relative humidity and vibration was proposed, and the data processing methods related to life evaluation were given. Using this method, the life of a certain silicone rubber thermal protective coating in the service environment is evaluated to be no less than 10 years, verifying the rationality and effectiveness of this method.

Key words

air-launched missile / thermal protective coating / service environment profile / life / evaluation method

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ZHANG Kai, YANG Mingjia, YANG Xiaokui, SHI Haobo. Life Evaluation of Thermal Protective Coatings for Air-launched Missiles[J]. Equipment Environmental Engineering. 2026, 23(1): 17-24 https://doi.org/10.7643/ issn.1672-9242.2026.01.003

References

[1] 姜贵庆, 马淑雅.防热涂层材料热防护性能预测[J].空气动力学学报, 2004, 22(1): 24-28.
JIANG G Q, MA S Y.The Prediction of Thermal Protection Performance for Coating Material[J].Acta Aerodynamica Sinica, 2004, 22(1): 24-28.
[2] 肖军, 陈建敏, 廖志忠, 等.弹体热防护涂层材料及制造技术工程实践[J].中国表面工程, 2025, 38(2): 442-453.
XIAO J, CHEN J M, LIAO Z Z, et al.Engineering Practice of Thermal Protective Coating Materials and Manufacturing Technology for Airborne Missile Bodies[J].China Surface Engineering, 2025, 38(2): 442-453.
[3] 李琳, 朱小飞, 杨科, 等.国内外战术导弹外防护涂层技术现状与发展趋势[J].航空制造技术, 2016, 59(14): 47-51.
LI L, ZHU X F, YANG K, et al.Progress in External Ablation-Resistant Coating for Tactical Missile[J].Aeronautical Manufacturing Technology, 2016, 59(14): 47-51.
[4] 肖军, 樊来恩, 曾一兵.高速空空导弹外防热涂层选用及试验[J].材料保护, 2022, 55(3): 157-161.
XIAO J, FAN L E, ZENG Y B.Selection and Experiment of Outer Thermal Protective Coatings for High-Speed Air-to-Air Missiles[J].Materials Protection, 2022, 55(3): 157-161.
[5] 吴江.飞航导弹热防护技术发展趋势[J].强度与环境, 2009, 36(1): 57-63.
WU J.Development of Thermal Protection Techniques for Aerodynamic Missile[J].Structure & Environment Engineering, 2009, 36(1): 57-63.
[6] 邹军锋, 李文静, 刘斌, 等.飞行器用热防护材料发展趋势[J].宇航材料工艺, 2015, 45(4): 10-15.
ZOU J F, LI W J, LIU B, et al.Development of Thermal Protection Materials for Aircraft[J].Aerospace Materials & Technology, 2015, 45(4): 10-15.
[7] 王开石, 匡松连.航天飞行器热防护涂层研究进展[J].宇航材料工艺, 2016, 46(6): 1-5.
WANG K S, KUANG S L.Developments of Coating Materials in the Thermal Protection System of Spacecrafts[J].Aerospace Materials & Technology, 2016, 46(6): 1-5.
[8] 陈万创, 李爱国.空空导弹综合环境可靠性试验剖面研究[J].上海航天, 2005(4): 41-44.
CHEN W C, LI A G.Research on Air to Air Missile Combined Environment Reliability Test Profile[J].Aerospace Shanghai, 2005(4): 41-44.
[9] 中国人民解放军总装备部.可靠性鉴定和验收试验: GJB 899A—2009[S].北京: 中国标准出版社, 2009.
General Armaments Department of the People's Liberation Army.Reliability Testing for Qualification and Production Acceptance: GJB 899A—2009[S].Beijing: Standards Press of China, 2009.
[10] 张仕念, 吴勋, 颜诗源, 等.贮存使用环境对导弹性能的影响机理[J].装备环境工程, 2014(5): 17-22.
ZHANG S N, WU X, YAN S Y, et al.Influencing Mechanism of Storage/Use Environment on Missile Performance[J].Equipment Environmental Engineering, 2014(5): 17-22.
[11] 魏仲委, 肖军, 刘建杰, 等.机载导弹弹体隔热层的热应力故障与对策[J].航空兵器, 2006, 13(2): 50-52.
WEI Z W, XIAO J, LIU J J, et al.Thermal Stress Failure on Heat Insulation Coatings for Airborne Missile Fuselage Connection[J].Aero Weaponry, 2006, 13(2): 50-52.
[12] 周益春, 刘奇星, 杨丽, 等.热障涂层的破坏机理与寿命预测[J].固体力学学报, 2010, 31(5): 504-531.
ZHOU Y C, LIU Q X, YANG L, et al.Failure Mechanisms and Life Prediction of Thermal Barrier Coatings[J].Chinese Journal of Solid Mechanics, 2010, 31(5): 504-531.
[13] 杨丽, 周益春, 齐莎莎.热障涂层的冲蚀破坏机理研究进展[J].力学进展, 2012, 42(6): 704-721.
YANG L, ZHOU Y C, QI S S.Research Progress in Erosion Mechanisms of Thermal Barrier Coatings[J].Advances in Mechanics, 2012, 42(6): 704-721.
[14] MILLER R A.Oxidation-Based Model for Thermal Barrier Coating Life[J].Journal of the American Ceramic Society, 1984, 67(8): 517-521.
[15] BUSSO E P, LIN J, SAKURAI S.A Mechanistic Study of Oxidation-Induced Degradation in a Plasma-Sprayed Thermal Barrier Coating System.Part II: Life Prediction Model[J].Acta Materialia, 2001, 49(9): 1529-1536.
[16] 耿瑞.热障涂层强度分析及寿命预测研究[D].北京: 北京航空航天大学, 2000.
GENG R.Analysis of Thermal Barrier Coatings and Life Prediction[D].Beijing: Beihang University, 2000.
[17] 杨晓光, 耿瑞, 周燕佩.热障涂层热疲劳寿命预测方法研究[J].航空动力学报, 2003, 18(2): 201-205.
YANG X G, GENG R, ZHOU Y P.A Study of Thermal Fatigue Life Prediction of TBC[J].Journal of Aerospace Power, 2003, 18(2): 201-205.
[18] 魏洪亮, 杨晓光, 齐红宇, 等.等离子涂层热疲劳失效模式及失效机理研究[J].航空动力学报, 2008, 23(2): 270-275.
WEI H L, YANG X G, QI H Y, et al.Study of Failure Mode and Failure Mechanisms on Thermal Fatigue of Plasma Sprayed Thermal Barrier Coatings[J].Journal of Aerospace Power, 2008, 23(2): 270-275.
[19] 宋佳楠, 李少林, 齐红宇, 等.热障涂层失效行为与寿命预测研究进展[J].航空制造技术, 2019, 62(3): 34-40.
ONG J N, LI S L, QI H Y, et al.Research on Failure Behavior and Life Prediction of Thermal Barrier Coatings[J].Aeronautical Manufacturing Technology, 2019, 62(3): 34-40.
[20] 中国人民解放军总装备部.装备环境工程通用要求: GJB 4239—2001[S].北京: 中国标准出版社, 2001.
General Armaments Department of the People's Liberation Army.General Requirements for Equipment Environmental Engineering: GJB 4239—2001[S].Beijing: Standards Press of China, 2001.
[21] 张生鹏, 李宏民, 赵朋飞.导弹装备贮存寿命加速试验技术体系探讨[J].装备环境工程, 2018, 15(2): 92-96.
ZHANG S P, LI H M, ZHAO P F.Accelerated Testing Technology System for Storage Life of Missile Equipment[J].Equipment Environmental Engineering, 2018, 15(2): 92-96.
[22] 李泽华.基于弦函数的温湿度耦合加速贮存试验模型构建方法: CN108763842A[P].2018-11-06.
LI Z H.Construction Method of Temperature and Humidity Coupled Accelerated Storage Test Model Based on Chord Function: CN108763842A[P].2018-11-06.
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