Hypersonic Boost-Glide Weapons

IF 0.7 Q3 INTERNATIONAL RELATIONS
J. Acton
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引用次数: 47

Abstract

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 ratio—a key performance parameter—is 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.
高超音速助推滑翔武器
美国、俄罗斯和中国正在开发高超音速助推滑翔飞行器。假设飞行器在过渡到平衡滑翔时不振荡,建立了一个简单的轨迹模型。该模型用于分析美国国防部高超音速技术飞行器-2试飞数据。这架滑翔机的升阻比——一个关键的性能参数——估计为2.6。该模型还用于计算助推滑翔攻击对敌方的战术预警时间。探讨了助推滑翔武器军事效能的其他方面。近似计算表明,与现有的非核武器相比,助推滑翔武器可以穿透更深,但在摧毁发射井方面效果较差。还计算了配备粒子扩散弹头的助推滑翔武器摧毁机动导弹的距离;预计它将比爆炸弹头大得多。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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来源期刊
Science & Global Security
Science & Global Security INTERNATIONAL RELATIONS-
CiteScore
1.00
自引率
14.30%
发文量
8
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