Development of a single-stage implosion-driven hypervelocity launcher

被引:0
|
作者
Szirti, Daniel [1 ]
Loiseau, Jason [1 ]
Batchelor, Patrick [1 ]
Higgins, Andrew J. [1 ]
Tanguay, Vincent [2 ]
Zhang, Fan [3 ]
机构
[1] McGill Univ, Dept Mech Engn, 817 Sherbrooke W,MacDonald Engn Bldg,Room 053, Montreal, PQ H3A 2K6, Canada
[2] Def R&D Canada Valcartier, Quebec City, PQ G3J 1X5, Canada
[3] Def R&D Canada Suffield, Medicine Hat, AB T1A 8K6, Canada
关键词
hypervelocity launcher; implosion; light gas gun;
D O I
暂无
中图分类号
O469 [凝聚态物理学];
学科分类号
070205 ;
摘要
Work, carried out on the development of a single-stage implosion-driven hypervelocity launcher is presented. Explosives surrounding a thin-walled tube filled with helium works similar to the pump tube of a conventional light gas gun. Implosion of the tube drives a strong shock that reflects back and forth between the projectile and the implosion pinch., generating very high temperatures and pressures. Experiments to evaluate the implosion dynamics and performance of the pump tube were carried out, with attention given to the helium fill pressure, diameter of the pump tube, thickness of the explosive layer, and the presence of a tamper. Simple analytic models were used to approximate the performance of the launcher; their advantages and limitations are discussed. Experiments with an implosion-driven launcher demonstrated muzzle velocities of 4 km/s with 5-mm-diameter aluminum projectiles, agreement with analytical models of performance is discussed. Projectile integrity was verified by high-speed photograph), and other diagnostics.
引用
收藏
页码:1147 / +
页数:2
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