Russian Nuclear Rocket Engine Design for Mars Exploration

被引:16
|
作者
Tsinghua Space Center, School of Aerospace, Tsinghua University, Beijing, 100084, China [1 ]
不详 [2 ]
机构
来源
Tsinghua Sci. Tech. | 2007年 / 3卷 / 256-260期
关键词
14;
D O I
10.1016/S1007-0214(07)70038-X
中图分类号
学科分类号
摘要
引用
收藏
相关论文
共 50 条
  • [41] DESIGN OPTIMIZATION OF SPLITTER BLADES FOR ROCKET ENGINE TURBOPUMP
    Torre, Francesco
    Konno, Shinichi
    Lettieri, Claudio
    Pini, Matteo
    Kawata, Yutaka
    PROCEEDINGS OF THE ASME TURBO EXPO: TURBOMACHINERY TECHNICAL CONFERENCE AND EXPOSITION, 2018, VOL 2D, 2018,
  • [42] Design of inlet for combined rocket-ramjet engine
    Zhao, Keyun
    Tuijin jishu, 1992, (05): : 34 - 37
  • [43] NOMOGRAPHIC MODEL FOR MULTICRITERIA OPTIMIZATION IN ROCKET ENGINE DESIGN
    DAUTOV, EA
    IZVESTIYA VYSSHIKH UCHEBNYKH ZAVEDENII AVIATSIONAYA TEKHNIKA, 1992, (01): : 88 - 91
  • [44] Fluorine Rocket Engine Demonstrators: Design, Tests, and Results
    Rothmund, Christophe
    HISTORY OF ROCKETRY AND ASTRONAUTICS, 2012, 37 : 315 - 336
  • [45] Preliminary design of a university laboratory hybrid rocket engine
    Trumpour A.
    Greatrix D.
    Karpynczyk J.
    Cherrington W.
    Canadian Aeronautics and Space Journal, 2010, 56 (01): : 1 - 8
  • [46] A new system design tool for a hybrid rocket engine
    Granado, Elena Quero
    Hijlkema, Jouke
    Lestrade, Jean-Yves
    Anthoine, Jerome
    ACTA ASTRONAUTICA, 2024, 223 : 119 - 133
  • [47] Influence of rocket design parameters on engine nozzle efficiencies
    Manski, D
    Hagemann, G
    JOURNAL OF PROPULSION AND POWER, 1996, 12 (01) : 41 - 47
  • [48] Reusable sounding rocket engine design and manufacturing status of development engine and components
    Hiraki, Hiromichi
    Niu, Ken-Ichi
    Kaneko, Takao
    Naruo, Yoshihiro
    Sato, Masaki
    Hashimoto, Tomoyuki
    Proceedings of the International Astronautical Congress, IAC, 2012, 9 : 7218 - 7226
  • [49] A carbon dioxide thermal rocket that utilizes an indigenous resource in raw form for Mars exploration
    Yu, D-R
    Lv, X-W
    Qin, J.
    Bao, W.
    Yao, Z-L
    PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 2010, 224 (G3) : 271 - 281
  • [50] ROCKET ENGINE
    HOLMES, R
    NAVAL ENGINEERS JOURNAL, 1968, 80 (01) : 144 - &