公开(公告)号：US20050116652A1

公开(公告)日：2005-06-02

申请号：US10726398

申请日：2003-12-02

申请人： John McVey ,  Andrew Perrucci ,  Edward Britt

发明人： John McVey ,  Andrew Perrucci ,  Edward Britt

IPC分类号： F03H1/00 ,  H01J7/24

CPC分类号： F03H1/0075

摘要： A Hall effect thruster for propelling spacecraft and satellites includes at least two acceleration channels, each of the channels has a closed end and an open end, and a plurality of flux guides adjacent each of the channels. The plurality of flux guides includes an innermost flux guide, an outermost flux guide, and at least one intermediate flux guide. Each intermediate flux guide helps provide a magnetic field to each of two adjacent acceleration channels.

摘要翻译： 用于推进航天器和卫星的霍尔效应推进器包括至少两个加速通道，每个通道具有封闭端和开口端，以及与每个通道相邻的多个通量引导件。 多个磁通引导件包括最内部的磁通引导件，最外面的磁通引导件和至少一个中间磁通引导件。 每个中间磁通引导件有助于为两个相邻加速度通道中的每一个提供磁场。

公开(公告)号：US06412275B1

公开(公告)日：2002-07-02

申请号：US09658138

申请日：2000-09-08

申请人： Andrew Perrucci

发明人： Andrew Perrucci

IPC分类号： F02K928

CPC分类号： F02K9/805 ,  F02K9/80 ,  F02K9/86 ,  F42B10/66

摘要： A solid divert and attitude control system for use on a kill vehicle or missile that includes a solid propellant gas generator, a control valve for modulating the effective exit area of the solid propellant gas generator, and a controller for calculating the integral of the burn rate of the solid propellant and for controlling operation of the control valve in response to the calculation of the integral of the burn rate of the solid propellant. The solid propellant gas generator has a solid propellant with a non-constant burn area and a grain profile which includes a first boost phase grain, an intermediate sustain phase grain, and a second boost phase. The controller controls operation of the control valve during a coast phase of the mission so that the second boost phase grain does not ignite until the beginning of the terminal phase of the mission.

摘要翻译： 一种用于杀伤车辆或导弹的固体转向和姿态控制系统，包括固体推进剂气体发生器，用于调节固体推进剂气体发生器的有效出射面积的控制阀，以及用于计算燃烧率积分的控制器 的固体推进剂，并且用于根据计算固体推进剂的燃烧速率的积分来控制控制阀的操作。 固体推进剂气体发生器具有固体推进剂，其具有不恒定的燃烧区域和包括第一升压相晶粒，中间维持相晶粒和第二升压阶段的晶粒轮廓。 控制器在任务的海岸阶段期间控制控制阀的操作，使得第二增压阶段颗粒在任务的最后阶段开始之前不会点燃。