In-Tube Rocket Propulsion Using Repetitive Laser Pulses  

作　　者：Akihiro Sasoh 

机构地区：[1]Department of Aerospace Engineering,Nagoya University,Furo-cho,Chikusa-ku,Nagoya 464-8603,Japan

出　　处：《Journal of Thermal Science》2011年第3期201-204,共4页热科学学报（英文版）

摘　　要：In 'in-tube propulsion,' that is the combination of conventional rocket propulsion and ballistic range operation,propulsion performance can be enhanced with increases in thrust due to spatial confinement and in payload capa-bility because propellant can be placed off board a projectile.This paper describes proofed concepts of in-tube propulsion by using repetitive laser pulses.

关 键 词：PROPULSION LASER THRUST Blast wave Ablation 

分 类 号：V430[航空宇航科学与技术—航空宇航推进理论与工程]