New Approaches for Human Deep-Space Exploration

被引:3
|
作者
Dunham, David W. [1 ,2 ]
Farquhar, Robert W. [1 ]
Eismont, Natan [3 ]
Chumachenko, Eugene [2 ]
机构
[1] KinetX Inc, Tempe, AZ 85284 USA
[2] Natl Res Univ, Higher Sch Econ, Moscow Inst Elect & Math, Moscow 109028, Russia
[3] Russian Acad Sci, Space Res Inst, Moscow 117997, Russia
来源
JOURNAL OF THE ASTRONAUTICAL SCIENCES | 2013年 / 60卷 / 02期
关键词
Human space exploration; Libration-point orbits; Gravity assist trajectories; Near-Earth Asteroids; Mars; MISSIONS; EARTH;
D O I
10.1007/s40295-014-0025-x
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
We are undertaking a Russian-American study of orbital options to extend human exploration beyond the Moon's orbit. For a viable program, an international collaboration (as now for the ISS) and reusable spacecraft will be needed. With reusable spacecraft, high-energy Earth orbits can be drastically modified with lunar swingbys and small maneuvers near the edge of the Earth's gravitational sphere of influence, especially near the collinear Sun-Earth and Earth-Moon libration points, to reach desired destinations. The work will build on ideas developed by the International Academy of Astronautics' exploration study group presented at the 2008 International Astronautical Congress in Glasgow. The first efforts could support backside lunar exploration from an Earth-Moon L2 temporary Lissajous or relatively permanent halo orbit; some quick low post-launch Delta V trajectories are presented. In a stepping stone approach, later missions could service large space telescopes near the Sun-Earth L2 libration point; explore near-Earth asteroids; and then the moons of Mars. The study will use highly-elliptical Earth orbits whose line of apsides can be rotated using lunar swingbys; then a propulsive maneuver, considerably smaller than that needed from a circular low-Earth orbit, can be applied at the right perigee to send the spacecraft on the right departure asymptote to a desired destination.
引用
收藏
页码:149 / 166
页数:18
相关论文
共 50 条
  • [1] New Approaches for Human Deep-Space Exploration
    David W. Dunham
    Robert W. Farquhar
    Natan Eismont
    Eugene Chumachenko
    The Journal of the Astronautical Sciences, 2013, 60 : 149 - 166
  • [2] A REUSABLE SYSTEM FOR DEEP-SPACE EXPLORATION
    LAFRAMBOISE, JG
    MIDDLETO.GI
    JOURNAL OF SPACECRAFT AND ROCKETS, 1970, 7 (05) : 598 - +
  • [3] Application of mass spectrometer in deep-space exploration
    Zhou, Zhi-Quan
    Lv, Hao
    Zhang, Dong
    Chen, Huan-Wen
    Zhao, Zhan-Feng
    Journal of Chinese Mass Spectrometry Society, 2015, 36 (06) : 492 - 505
  • [4] China's Deep-space Exploration to 2030
    ZOU Yongliao
    LI Wei
    OUYANG Ziyuan
    空间科学学报, 2014, (05) : 516 - 517
  • [5] CHINA'S MARS LAUNCH SEALS NEW ERA IN DEEP-SPACE EXPLORATION
    Mallapaty, Smriti
    NATURE, 2020, 583 (7818) : 671 - 671
  • [6] SMART COMMUNICATIONS AND NETWORKING FOR FUTURE DEEP-SPACE EXPLORATION
    Zhang, Qinyu
    Sun, Zhili
    de Cola, Tomaso
    Zhao, Kanglian
    CHINA COMMUNICATIONS, 2020, 17 (07) : III - VI
  • [7] CVN software correlator applications in deep-space exploration
    Zheng Weimin
    Shu Fengchun
    Dong, Zhang
    SECOND INTERNATIONAL CONFERENCE ON SPACE INFORMATION TECHNOLOGY, PTS 1-3, 2007, 6795
  • [8] Application of nuclear photon engines for deep-space exploration
    Gulevich, AV
    Ivanov, EA
    Kukharchuk, OF
    Poupko, VY
    Zrodnikov, AV
    SPACE TECHNOLOGY AND APPLICATIONS INTERNATIONAL FORUM-2001, 2001, 552 : 957 - 962
  • [9] SMART COMMUNICATIONS AND NETWORKING FOR FUTURE DEEP-SPACE EXPLORATION
    Qinyu Zhang
    Zhili Sun
    Tomaso de Cola
    Kanglian Zhao
    中国通信, 2020, 17 (07) : 6 - 9
  • [10] A fast scanning method for deep-space exploration antennas
    Cao, Hai-Lin
    Yang, Li-Sheng
    Tan, Xiao-Heng
    Yang, Shi-Zhong
    Chongqing Daxue Xuebao/Journal of Chongqing University, 2010, 33 (12): : 127 - 132