An Impulse Thruster for Radial Thrust Trajectory Correction

• 作 者: 杨庆 汪佩兰 王丽琼 金建峰 安尼瓦尔
• 机 构: StateKeyLaboratoryofExplosionScienceandTechnology,HuayinOrdnanceTestCentre
• 出 处: Journal of China Ordnance
• 发表日期: 2008年4期
• 关键词: 火工品 光线 弹道 问题 physical chemistry radial thrust trajectory correction impulse thru

A prototype of impulse thruster for radial thrust trajectory correction munitions is designed. It adopts semiconductor bridge (SCB) as ignition element,Ti/KClO4 (TK) as ignition charge and ammonium perchlorate/aluminium (NA) or potassium picate/RDX (KR) a