NEW RADIATOR SYSTEM DESIGNED FOR LARGE SPACECRAFT.

被引：0
|
作者：
Anon
机构：
来源：
Aerospace Engineering (Warrendale, Pennsylvania) | 1988年 / 8卷 / 01期
关键词：
D O I：
暂无
中图分类号：
学科分类号：
摘要：
引用
收藏
页码：52 / 56
相关论文
共 50 条
  • [1] NUCLEAR THERMIONIC POWER SYSTEM FOR SPACECRAFT.
    Phillips, W.M.
    Estabrook, W.C.
    Hsieh, T.M.
    1976, 2 SAE : 1487 - 1493
  • [2] ISPM SPACECRAFT.
    Wenzel, K.-P.
    European Space Agency, (Special Publication) ESA SP, 1983, : 277 - 293
  • [3] VOYAGER SPACECRAFT.
    Heacock, Raymond L.
    Proceedings - Institution of Mechanical Engineers, 1980, 194 : 211 - 224
  • [4] SYSTEM DESIGN OF JAPANESE FIRST INTERPLANETARY SPACECRAFT.
    Hirao, Kunio
    Hayashi, Tomonao
    Uesugi, Kuninori
    Itoh, Tomizo
    Hara, Hironori
    Yamamoto, Harumitsu
    Masumoto, Yoshinari
    Orii, Takeshi
    Kamimura, Masayuki
    NEC Research and Development, 1986, (81): : 24 - 31
  • [5] AMPTE CCE SPACECRAFT.
    Dassoulas, John
    Margolies, Donald L.
    Peterson, Max
    IEEE Transactions on Geoscience and Remote Sensing, 1985, GE-23 (03): : 182 - 191
  • [6] DYNAMICS OF GYROELASTIC SPACECRAFT.
    D'Eleuterio, G.M.T.
    Hughes, P.C.
    Journal of Guidance, Control, and Dynamics, 1987, l0 (04)
  • [7] DESIGN OF STRUCTURES FOR SPACECRAFT.
    Patrick, Tom
    Space education, 1985, 1 (09): : 418 - 422
  • [8] ELECTRIC PROPULSION OF SPACECRAFT.
    Fearn, D.G.
    JBIS. Journal of the British Interplanetary Society, 1982, 35 (04): : 156 - 166
  • [9] INTELSAT IV SPACECRAFT.
    Jilg, E.T.
    1600, (02):
  • [10] DEVELOPMENT OF AN EXPERT SYSTEM FOR THE COMMAND AND CONTROL OF AN ORBITING SPACECRAFT.
    Harris, Henry M.
    The Journal of Forth application and research, 1986, 4 (02):
12345