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Aerospace laser ignition/ablation variable high precision thruster

机译:航天激光点火/烧蚀可变高精度推进器

摘要

A laser ignition/ablation propulsion system that captures the advantages of both liquid and solid propulsion. A reel system is used to move a propellant tape containing a plurality of propellant material targets through an ignition chamber. When a propellant target is in the ignition chamber, a laser beam from a laser positioned above the ignition chamber strikes the propellant target, igniting the propellant material and resulting in a thrust impulse. The propellant tape is advanced, carrying another propellant target into the ignition chamber. The propellant tape and ignition chamber are designed to ensure that each ignition event is isolated from the remaining propellant targets. Thrust and specific impulse may by precisely controlled by varying the synchronized propellant tape/laser speed. The laser ignition/ablation propulsion system may be scaled for use in small and large applications.
机译:激光点火/烧蚀推进系统具有液体和固体推进的优点。卷盘系统用于使包含多个推进剂靶材的推进剂带移动通过点火室。当推进剂靶位于点火室内时,来自位于点火室上方的激光器的激光束撞击推进剂靶,从而点燃推进剂材料并产生推力脉冲。推进推进剂带,将另一个推进剂目标带入点火室。推进剂带和点火室的设计确保每次点火都与其余推进剂靶隔离。推力和比冲可通过改变同步推进剂带/激光速度来精确控制。激光点火/烧蚀推进系统可以按比例缩放以用于小型和大型应用。

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