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公开(公告)号:KR1020110128394A
公开(公告)日:2011-11-30
申请号:KR1020100047818
申请日:2010-05-24
Applicant: 국방과학연구소
Abstract: PURPOSE: A plasma injector for igniting a propellant is provided to reduce the ignition delay time of a propellant by stably injecting high-temperature and high-pressure plasma to the propellant. CONSTITUTION: A plasma injector for igniting a propellant comprises an injector body(11), inner and outer electrodes(12,13), insulating units(18,19), a capillary tube(14), a metal wire(15), an ablation material(16), and a plug(17). The inner and outer electrodes and the insulating units are installed inside the injector body and transfer high-power pulse electric energy to the injector body. The capillary tube is formed in the inner center of the injector body and generates plasma from the electric energy. The metal wire crosses the capillary tube. The ablation material is installed in the edge of the metal wire. The plug seals one end of the injector body.
Abstract translation: 目的:提供一种用于点燃推进剂的等离子体注入器,通过将高温和高压等离子体稳定地注入到推进剂中来减少推进剂的点火延迟时间。 构成:用于点燃推进剂的等离子体注入器包括喷射器主体(11),内外电极(12,13),绝缘单元(18,19),毛细管(14),金属丝(15), 消融材料(16)和插头(17)。 内外电极和绝缘单元安装在注射器主体内部,并将大功率脉冲电能传递到喷射器主体。 毛细管形成在喷射器主体的内部中心,并从电能产生等离子体。 金属丝穿过毛细管。 烧蚀材料安装在金属丝的边缘。 插头密封注射器主体的一端。