ZENG Zhaohuan. Aerospace Mater Technol (in Chinese), 1989, 19(3): 12–20.
[7]
？ 郭正, 赵稼祥. 碳碳复合材料的研究与发展[J]. 宇航工艺材料, 1995(5): 1–7.
[8]
GUO Zhen, ZHAO Jiaxiang. Aerospace Mater Technol (in Chinese), 1995(5): 1–7.
[9]
？ RUDY E. Compendium of phase diagram data: ternary phase equilibr ia in transition metal-boron-carbon-silicon systems Part 5 - air force materials laboratory, wright - patterson air force base [R]. Ohio, 1969.
[10]
？ SYLVIA M, Johnson and MATTTHEW J. Gasch, DAN Leiser, DAVID Stewart, Jr. Development of new TPS at NASA Ames Research Center [R]. AIAA, 2008–2560.
[11]
？ DAVID A S, DANIEL B L. Lightweight TUFROC TPS for Hypersonic Vehicles [R]. Canberra, AIAA 20067945.
SU Fang, MENG Xianhong. Aerodynamic Missile (in Chinese), 2006(10): 57–60.
[17]
？ RONAILD P B. Rigid fibrous ceramics for entry systems [R]. NASA N93-22117: 431–437.
[18]
？ FROSH R A, LEISER D B, GOLDSTEIN H E, et al. Fibrous refractory composite insulation [P]. US Patent, 4 148 962. 1979–04–10.
[19]
？ MARSHELL B A. Space shuttle FRCI-12 TPS tile venting test in the NASA/AMES research center 11X11-foot and 9X7-foot wind tunnels [R]. 1982, NASA–CR–167.
LIU Luowei. Aerodyn Missle (in Chinese), 2003(12): 54–55.
[22]
？ EHRLICH C F. TPS/Insulation concepts for vehicles with reusable cryotanks [R]. 1994, AIAA–94–4675.
[23]
？ LEISER D B, SMITH M, STEWART D A. Options for improving rigidized ceramic heat shields [J]. Ceram Eng Sci Proc, 1985(6): 757–768.
[24]
？ LEISER D B, SMITH M, STEWARD D A. Effect of fiber size and composition on mechanical and thermal properties of low density ceramic composite insulation materials [R]. NASA CP, 1984, 2357: 231–244.
[25]
？ DICHIARAR A. Method of making apermeable ceramic tile insulation [P]. Patent US 6 613 255 B2. 2003–09–02.
[26]
？ STEWART D A, LEISER D B, SMITH M. Thermal response of integral multicomponent composite thermal protection systems [R]. AIAA–85–1056.
[27]
？ YU J, KWAN H W. Use of HTP ceramic foam for aeroacoustic applications [R]. AIAA–97–1705–CP: 887–897.
[28]
？ BANAS R P, CREEDON J F, CUNNINGTON J R. Thermophysical and mechanical properties of the HTP family of rigid ceramic insulation materials [R]. AIAA–85–1055, 1985.
[29]
？ HENG V, HINKLE K A, SANTOS M A. Rigid insulation and method of producing same [P]. US Patent 6, 716, 782 B2. 2004–04–06.
[30]
？ MAAHS H G, VAUGHN W I, KOWEL W. Four advances in carborr-carbon materials technology [R]. 1994, NASA N94–304811–15.
[31]
？ RODRIGU A C, SNAPP C G. Orbiter Thermal Protection System Lessons Learned [R]. AIAA, 2011–7308.
[32]
？ 竺士伟. 航天飞机热结构反思[J]. 太空探索, 2011(1): 26–34.
[33]
ZHU Shiwei. Space Exploration (in Chinese), 2011(1): 26–34.
LI Junning, HU Zijun, SUNChencheng, et al. Aerospace Mater Technol (in Chinese), 2011(6): 10–13.
[36]
？ PHILIP T, HARSHI, LOEWELL C Keel. X-43A vehicle design and manufacture [R]. AIAA, 2005–3334.
[37]
？ KEVIN RIVERS H, DAVID E. Glass, advances in hot-structure development [R]. AIAA, 20060020757.
[38]
？ DANIEL B. Leiser, DAVID A. Stewart, ROBERT DiFiore, Flight performance of a functionally gradient Material TUFI on Shuttle Orbiter [R]. NASA–20020042186.
[39]
？ DANIEL B L, MASHNELL Smith, et al. Toughened uni-piece fibrous Insulation [P]. US Patent 5, 079082, 1992–01–07.
[40]
？ MILOS F S, SQUIRE T H. Thermal stress analysis of X-34 wing leading edge tile TPS [R]. 1996, AIAA–96–1821.
[41]
？ STEWART D A, DANIEL B L, ROBERT R D, et al. High efficiency tantalum-based ceramic composite structures [P]. US patent, 7.767, 303131, 2010–08–03.
PEI Yuchen, LI Wenjing, ZHANG Fan, et al. Aerodyn Missile (in Chinese), 2012(3): 93–96.
[48]
？ SYLVIA M J, MATT G, JOHN W L. Recent Developments in Ultra High Temperature Ceramics at NASA Ames [R]. AIAA 2009–7219.
[49]
？？ DAVID A, Steward, SANTA Cruz, DANIEL B, Leiser, Toughened uni-piece, fibrous, reinforced, oxidization-resistant composite [P]. US Patent 7, 381, 459 B1, 2008–06–03.
