Hypersonic Boost-Glide Weapons

被引:52
|
作者
Acton, James M. [1 ]
机构
[1] Carnegie Endowment Int Peace, Nucl Policy Program, 1779 Massachusetts Ave NW, Washington, DC 20036 USA
关键词
This work was primarily funded by the John D. and Catherine T. MacArthur Foundation; with supplementary support from the William and Flora Hewlett Foundation and the Carnegie Corporation of New York;
D O I
10.1080/08929882.2015.1087242
中图分类号
D81 [国际关系];
学科分类号
030207 ;
摘要
The United States, Russia and China are developing hypersonic boost-glide vehicles. A simple model of their trajectory is developed by assuming that the vehicle does not oscillate during the transition to equilibrium gliding. This model is used to analyze U.S. Department of Defense data on test flights for the Hypersonic Technology Vehicle-2. This glider's lift-to-drag ratioa key performance parameteris estimated to be 2.6. The model is also used to calculate the tactical warning time that a boost-glide attack would afford an adversary. Other aspects of boost-glide weapons' military effectiveness are explored. Approximate calculations suggest that, compared to existing non-nuclear weapons, boost-glide weapons could penetrate more deeply but would be less effective at destroying silos. The distance at which a boost-glide weapon armed with a particle dispersion warhead could destroy a mobile missile is also calculated; it is expected to be significantly larger than for an explosive warhead.
引用
收藏
页码:191 / 219
页数:29
相关论文
共 50 条
  • [41] Global Strike Hypersonic Weapons
    Lewis, Mark J.
    NUCLEAR WEAPONS AND RELATED SECURITY ISSUES, 2017, 1898
  • [42] Hypersonic Weapons and Strategic Stability
    Wilkening, Dean
    SURVIVAL, 2019, 61 (05) : 129 - 148
  • [43] Analysis of uniqueness and optimality of glide segment initial state for hypersonic glide vehicle
    Meng F.
    Tian K.
    Guofang Keji Daxue Xuebao/Journal of National University of Defense Technology, 2020, 42 (05): : 115 - 125
  • [44] Ascent and Glide Trajectory Optimization for Hypersonic Vehicle
    Mahmoud, AbdelMageed
    Hao, Zhou
    Chen Wanchun
    Yang, Liang
    2017 INTERNATIONAL CONFERENCE ON CONTROL, ARTIFICIAL INTELLIGENCE, ROBOTICS & OPTIMIZATION (ICCAIRO), 2017, : 133 - 142
  • [45] Maneuver characteristics analysis for hypersonic glide vehicles
    Li, Guanghua
    Zhang, Hongbo
    Tang, Guojian
    AEROSPACE SCIENCE AND TECHNOLOGY, 2015, 43 : 321 - 328
  • [46] Control of Hypersonic Vehicles in Cruise and Glide Periods
    Yuan Jian
    Shi Bao
    Ji Wenqiang
    2013 32ND CHINESE CONTROL CONFERENCE (CCC), 2013, : 685 - 690
  • [47] Typical trajectory characteristics of hypersonic glide vehicle
    Li, Guang-Hua
    Zhang, Hong-Bo
    Tang, Guo-Jian
    Yuhang Xuebao/Journal of Astronautics, 2015, 36 (04): : 397 - 403
  • [48] Maneuver Modes Analysis for Hypersonic Glide Vehicles
    Li, Guanghua
    Zhang, Hongbo
    Tang, Guojian
    Xie, Yu
    2014 IEEE CHINESE GUIDANCE, NAVIGATION AND CONTROL CONFERENCE (CGNCC), 2014, : 543 - 548
  • [49] Virtual Displacement Guidance for Hypersonic Glide Vehicle
    Chen Erkang
    Gao Changsheng
    Jing Wuxing
    PROCEEDINGS OF THE 35TH CHINESE CONTROL CONFERENCE 2016, 2016, : 5301 - 5306
  • [50] Adaptive tracking method for hypersonic glide target
    Huang, Jingshuai
    Li, Yongyuan
    Tang, Guojian
    Bao, Weimin
    Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica, 2020, 41 (09):