Stages of Development of Cryogenic Systems for Space Rocket Technology

被引：0
|
作者：
Yu. V. Gorbatskii
A. M. Domashenko
V. N. Krishtal
机构：
[1] Open Joint-Stock Company,
来源：
Chemical and Petroleum Engineering | 2002年 / 38卷
关键词：
Cryogenic System; Rocket Technology; Space Rocket; Space Rocket Technology;
D O I：
暂无
中图分类号：
学科分类号：
摘要：
引用
收藏
页码：594 / 598
页数：4
相关论文
共 50 条
  • [21] MULTICRITERIAL COMPARATIVE ANALYSIS OF ROCKET AND SPACE TECHNOLOGY
    Gusynin, V. P.
    Goldshtein, Yu. M.
    Doroshkevich, V. K.
    Kuznetsov, V. I.
    Kuchugurny, Yu. P.
    SPACE SCIENCE AND TECHNOLOGY-KOSMICNA NAUKA I TEHNOLOGIA, 2005, 11 (1-2): : 3 - 9
  • [22] THE STATUS AND DIRECTIONS FOR IMPROVING THE REGULATORY AND PROCEDURAL FRAMEWORK FOR THE ROCKET AND SPACE TECHNOLOGY DEVELOPMENT IN UKRAINE
    Alpatov, A. P.
    Marchenko, V. T.
    Khorolskyi, P. P.
    Sazina, N. P.
    SCIENCE AND INNOVATION, 2022, 18 (01): : 76 - 88
  • [23] The Development and Application of Ground Systems and Derived Systems of Space Technology
    Yang Jiachi Xu Fangwen
    Aerospace China, 1993, (01) : 2 - 6
  • [24] ROCKET AS SPACECRAFT: SPENT STAGES IN MANNED SPACE FLIGHT.
    Compton, W.David
    JBIS. Journal of the British Interplanetary Society, 1985, 38 (04): : 147 - 154
  • [25] CRYOGENIC ROCKET PROPELLANTS
    DOUGLASS, HW
    MECHANICAL ENGINEERING, 1968, 90 (03) : 68 - &
  • [26] THE ROCKET - THE HISTORY AND DEVELOPMENT OF ROCKET AND MISSILE TECHNOLOGY - BAKER,D
    BURNS, ELM
    QUEENS QUARTERLY, 1981, 88 (01) : 174 - 175
  • [27] CRYOGENIC ROCKET PROPELLANTS
    DOUGLASS, HW
    MECHANICAL ENGINEERING, 1968, 90 (06) : 38 - &
  • [28] CRYOGENIC THERMOMETRY FOR SPACE TESTING SYSTEMS
    BLANPAIN, R
    JAMAR, C
    MACAU, JP
    CUCCHIARO, A
    CRYOGENICS, 1992, 32 : 226 - 228
  • [29] Space cryogenic systems model and capabilities
    Franck, RA
    Glaister, DG
    ADVANCES IN CRYOGENIC ENGINEERING, VOLS. 49A AND B, 2004, 710 : 1536 - 1545
  • [30] Risk management in space systems design and technology development
    Silk, E. A.
    Dash, P. H.
    PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 2008, 222 (G6) : 907 - 913
12345