Thermo-structural design of ZrB2–SiC-based thermal protection system for hypersonic space vehicles

被引:0
|
作者
机构
[1] Purwar, Anupam
[2] Basu, Bikramjit
来源
Basu, Bikramjit (bikram@mrc.iisc.ernet.in) | 1618年 / Blackwell Publishing Inc., Postfach 10 11 61, 69451 Weinheim, Boschstrabe 12, 69469 Weinheim, Deutschland, 69469, Germany卷 / 100期
关键词
51;
D O I
暂无
中图分类号
学科分类号
摘要
引用
收藏
相关论文
共 38 条
  • [1] Thermo-structural design of ZrB2-SiC-based thermal protection system for hypersonic space vehicles
    Purwar, Anupam
    Basu, Bikramjit
    JOURNAL OF THE AMERICAN CERAMIC SOCIETY, 2017, 100 (04) : 1618 - 1633
  • [2] Development of ZrB2-SiC Plasma-Sprayed Ceramic Coating for Thermo-chemical Protection in Hypersonic Vehicles
    Kalpana Gupta
    Qasim Murtaza
    N. Yuvraj
    Journal of Materials Engineering and Performance, 2024, 33 : 1401 - 1410
  • [3] Development of ZrB2-SiC Plasma-Sprayed Ceramic Coating for Thermo-chemical Protection in Hypersonic Vehicles
    Gupta, Kalpana
    Murtaza, Qasim
    Yuvraj, N.
    JOURNAL OF MATERIALS ENGINEERING AND PERFORMANCE, 2024, 33 (03) : 1401 - 1410
  • [4] Integrated thermal protection and control system design methodology for hypersonic vehicles
    Wang, Jun
    Wang, Peiguang
    Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics, 2006, 32 (10): : 1129 - 1134
  • [5] Design of Thermal Barrier Coating System for Scramjet using Coupled Thermo-Structural Analysis
    Purwar, Anupam
    Mahapatra, D. Roy
    TRANSACTIONS OF THE INDIAN CERAMIC SOCIETY, 2016, 75 (04) : 242 - 249
  • [6] Electrochemical Corrosion of Composite Ceramics and Thermal Spray Coatings in the ZrB2–SiC–AlN System
    O. N. Grigoriev
    V. A. Shvets
    I. A. Podchernyaeva
    D. V. Yurechko
    D. V. Vedel
    A. A. Zubarev
    I. V. Smirnov
    V. I. Kopylov
    V. N. Talash
    Yu. B. Rudenko
    Powder Metallurgy and Metal Ceramics, 2020, 59 : 394 - 400
  • [7] Mechanism of High-Temperature Oxidation of ZrB2-Based Composite Ceramics in the ZrB2–SiC–AlN System
    O. N. Grigoriev
    A. D. Panasyuk
    I. A. Podchernyaeva
    I. P. Neshpor
    D. V. Yurechko
    Powder Metallurgy and Metal Ceramics, 2018, 57 : 71 - 74
  • [8] OPTIMAL THERMAL DESIGN OF A MULTISHIELD THERMAL PROTECTION SYSTEM OF REUSABLE SPACE VEHICLES
    Maiorova, I. A.
    Prosuntsov, P. V.
    Zuev, A. V.
    JOURNAL OF ENGINEERING PHYSICS AND THERMOPHYSICS, 2016, 89 (02) : 528 - 533
  • [9] Multilayer SiC for thermal protection system of space vehicles with decreased thermal conductivity through the thickness
    Biamino, S.
    Antonini, A.
    Eisenmenger-Sittner, C.
    Fuso, L.
    Pavese, M.
    Fino, P.
    Bauer, E.
    Badini, C.
    JOURNAL OF THE EUROPEAN CERAMIC SOCIETY, 2010, 30 (08) : 1833 - 1840
  • [10] Six sigma robust design optimization for thermal protection system of hypersonic vehicles based on successive response surface method
    Jingjing ZHU
    Xiaojun WANG
    Haiguo ZHANG
    Yuwen LI
    Ruixing WANG
    Zhiping QIU
    Chinese Journal of Aeronautics, 2019, (09) : 2095 - 2108