Thermal analysis of the thermal protection system for the re-entry vehicle

被引：0
|
作者：
Natl Aerospace Lab, Tokyo, Japan [1 ]
机构：
来源：
Comput Methods Appl Mech Eng | / 3-4卷 / 301-310期
关键词：
D O I：
暂无
中图分类号：
学科分类号：
摘要：
引用
下载
收藏
相关论文
共 50 条
  • [1] Thermal analysis of the thermal protection system for the re-entry vehicle
    Ohtake, K
    COMPUTER METHODS IN APPLIED MECHANICS AND ENGINEERING, 1998, 151 (3-4) : 301 - 310
  • [2] Thermal analysis of re-entry vehicle structure
    Ohtake, K
    Endo, S
    Ogawa, S
    Haneji, K
    Kamohara, M
    SPACE COOPERATION INTO THE 21ST CENTURY, 1997, 96 : 923 - 932
  • [3] THERMAL PROTECTION OF A RE-ENTRY SATELLITE
    SCALA, SM
    ARS JOURNAL, 1959, 29 (09): : 670 - 672
  • [4] Aeroheating reduction by adaptive thermal protection structures for a re-entry vehicle
    Lampani, L
    Gaudenzi, P
    4TH EUROPEAN WORKSHOP ON HOT STRUCTURES AND THERMAL PROTECTION SYSTEMS FOR SPACE VEHICLES, 2003, 521 : 255 - 257
  • [5] DESIGN OF A CRUSHABLE THERMAL PROTECTION SYSTEM FOR THE EARTH RE-ENTRY CAPSULE
    Carvalho, Joao
    Ribeiro, Carlos
    Sa, Ricardo
    Marques, Angelo
    Carneiro, Filipa
    Chaves, Paulo
    Marques, Nuno
    Carrolo, Edgar
    Antunes, Paulo J.
    Viana, Julio C.
    Rebuffat, Denis
    Ngan, Ivan
    PROCEEDINGS OF THE 7TH INTERNATIONAL CONFERENCE ON MECHANICS AND MATERIALS IN DESIGN (M2D2017), 2017, : 63 - 80
  • [6] Beta-Titanium Alloy Thermal Protection System for Re-entry Vehicles
    Fischer, Wolfgang P. P.
    SAE INTERNATIONAL JOURNAL OF AEROSPACE, 2009, 1 (01): : 461 - 472
  • [7] Thermal protection of re-entry vehicles with the usage of inflatable systems
    Alifanov, OM
    Outchvatov, VI
    Pichkhadze, KM
    ACTA ASTRONAUTICA, 2003, 53 (4-10) : 541 - 546
  • [8] COMPOSITE THERMAL PROTECTION SYSTEMS FOR MANNED RE-ENTRY VEHICLES
    SWANN, RT
    ARS JOURNAL, 1962, 32 (02): : 221 - 226
  • [9] ROLE OF REFRACTORY THERMAL PROTECTION SYSTEMS IN BALLISTIC RE-ENTRY
    JAMES, DR
    AMERICAN CERAMIC SOCIETY BULLETIN, 1966, 45 (04): : 391 - &
  • [10] APPLICATION STATUS OF C/C COMPOSITES FOR THERMAL PROTECTION SYSTEM IN RE-ENTRY SPACECRAFT
    Sun Guoling
    Ji, Zhou
    HIGH TEMPERATURE CERAMIC MATRIX COMPOSITES 8: CERAMIC TRANSACTIONS, VOL 248, 2014, 248 : 461 - 464
12345