ABLATIVE THERMAL PROTECTION FOR SPACE TUG MULTIPASS, AEROBRAKING ENTRY

被引：3
|
作者：
STRAUSS, EL [1 ]
机构：
[1] MARTIN MARIETTA AEROSP,STRUCT & MAT DEPT,DENVER,CO 80200
来源：
JOURNAL OF SPACECRAFT AND ROCKETS | 1975年 / 12卷 / 06期
关键词：
D O I：
10.2514/3.56986
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
引用
收藏
页码：346 / 350
页数：5
相关论文
共 50 条
  • [31] Integrated computing method for ablative thermal protection system of reentry vehicles
    Zhou, Yinjia
    Zhang, Zhixian
    Fu, Xinwei
    A, Rong
    Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica, 2021, 42 (07):
  • [32] 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
  • [33] Thermal analysis of the thermal protection system for the re-entry vehicle
    Natl Aerospace Lab, Tokyo, Japan
    Comput Methods Appl Mech Eng, 3-4 (301-310):
  • [34] Design, qualification, manufacturing and integration of IXV Ablative Thermal Protection System
    Cioeta, Mario
    Di Vita, Gandolfo
    Maria, Teresa Signorelli
    Bianco, Gianluca
    Cutroni, Maurizio
    Damiani, Francesco
    Ferretti, Viviana
    Rotondo, Adriano
    ACTA ASTRONAUTICA, 2016, 124 : 90 - 101
  • [35] A model for thermal protection ablative material with local thermal non-equilibrium and thermal radiation mechanisms
    Li, Weijie
    Huang, Jie
    Zhang, Zhongwei
    Wang, Liyan
    Huang, Haiming
    Liang, Jun
    ACTA ASTRONAUTICA, 2021, 183 : 101 - 111
  • [36] THERMAL PROTECTION SYSTEMS FOR A MARS-ENTRY VEHICLE
    HILTZ, AA
    FLORENCE, DE
    LOWE, DL
    JOURNAL OF SPACECRAFT AND ROCKETS, 1968, 5 (11) : 1278 - &
  • [37] Thermal-Structural Coupled Analysis and Design of a Reentry Capsule with Ablative Thermal Protection Systems
    Park, Yerin
    Shin, Eui Sup
    INTERNATIONAL JOURNAL OF AERONAUTICAL AND SPACE SCIENCES, 2024,
  • [38] Three-Dimensional Finite Element Ablative Thermal Response and Design of Thermal Protection Systems
    Dec, John A.
    Braun, Robert D.
    JOURNAL OF SPACECRAFT AND ROCKETS, 2013, 50 (04) : 725 - 734
  • [39] Space shuttle thermal protection system
    Leiser, DB
    AMERICAN CERAMIC SOCIETY BULLETIN, 2004, 83 (08): : 44 - 47
  • [40] Synthesis, characterisation and qualification of high performance phenolic/carbon random-fibre oriented ablative thermal protection composite for re-entry applications
    Kumar, L. Mohan
    Chakravarthy, P.
    Anandapadmanabhan, E. N.
    INTERNATIONAL JOURNAL OF MATERIALS & PRODUCT TECHNOLOGY, 2022, 64 (01): : 23 - 35
12345