NEW ABLATIVE HEAT SHIELD MATERIALS FOR MARS LANDERS

被引:0
|
作者
STRAUSS, EL
机构
来源
SAE TRANSACTIONS | 1967年 / 75卷
关键词
D O I
暂无
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
引用
收藏
页码:134 / &
相关论文
共 50 条
  • [31] Highly filled organoclay/phenolic resin nanocomposite as an ablative heat shield material
    Azin Paydayesh
    Mehrdad Kokabi
    Iranian Polymer Journal, 2015, 24 : 389 - 397
  • [32] Arcjet screening of candidate ablative thermal protection materials for Mars Science Laboratory
    Laub, B
    White, S
    JOURNAL OF SPACECRAFT AND ROCKETS, 2006, 43 (02) : 367 - 373
  • [33] Reconstruction of Aerothermal Environment and Heat Shield Response of Mars Science Laboratory
    Bose, Deepak
    White, Todd
    Mahzari, Milad
    Edquist, Karl
    JOURNAL OF SPACECRAFT AND ROCKETS, 2014, 51 (04) : 1174 - 1184
  • [34] Transition due to heat-shield cavities on a Mars entry vehicle
    Hollis, BR
    Liechty, DS
    JOURNAL OF SPACECRAFT AND ROCKETS, 2006, 43 (02) : 354 - 366
  • [35] HEAT SHIELD MATERIALS KEY TO SPACE SHUTTLE
    KORB, LJ
    METAL PROGRESS, 1972, 101 (04): : 83 - &
  • [36] Low cost approach to mars pathfinder and small landers
    Spear, Anthony J.
    Acta Astronautica, 35 (Suppl):
  • [37] MARS ATMOSPHERIC CIRCULATION - ASPECTS FROM VIKING LANDERS
    RYAN, JA
    JOURNAL OF GEOPHYSICAL RESEARCH-SPACE PHYSICS, 1985, 90 (NA7): : 6319 - 6325
  • [38] APPROACH NAVIGATION FOR DELIVERY OF SMALL LANDERS TO THE SURFACE OF MARS
    HECHLER, M
    LAUER, M
    JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 1994, 17 (01) : 116 - 122
  • [39] Performance of a low density ablative heat shield material (vol 45, 237, 2008)
    Covington, M. A.
    Heinemann, J. M.
    Goldstein, H. E.
    Chen, Y. -K.
    Terrazas-Salinas, I.
    Balboni, J. A.
    Olejniczak, J.
    Martinez, E. R.
    JOURNAL OF SPACECRAFT AND ROCKETS, 2008, 45 (04) : 854 - 864
  • [40] Proposal for new space heat shield
    不详
    AMERICAN CERAMIC SOCIETY BULLETIN, 2009, 88 (07): : 33 - 33