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首页> 外文会议>International Astronautical Congress >CONTROLLABLE SOLID PROPULSION FOR LAUNCH VEHICLE AND SPACECRAFT APPLICATION PREPARED FOR THE 57~(TH) INTERNATIONAL ASTRONAUTICAL CONGRESS, OCTOBER 2006
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CONTROLLABLE SOLID PROPULSION FOR LAUNCH VEHICLE AND SPACECRAFT APPLICATION PREPARED FOR THE 57~(TH) INTERNATIONAL ASTRONAUTICAL CONGRESS, OCTOBER 2006

机译：为57〜（Th）国际宇航大会，2006年10月制定了57〜（Th）国际司机的发射车辆和航天器申请的可控固体推进

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Aerojet, a leading rocket and space propulsion company in the United States (US), has been developing controllable solid propellant propulsion systems for a wide variety of applications including systems in production. Controllable solid propulsion systems provide variable thrust capability with high turn-down ratios by changing the nozzle throat area and the motor's operating pressure during operation. Aerojet has developed numerous controllable systems with single and multiple variable thrust nozzles for axial propulsion rocket motors and attitude control systems, respectively. Recently, Aerojet began work on controllable thrust systems for crew launch vehicles and spacecraft applications in support of NASA's Space Exploration program. This paper provides an overview of Aerojet's controllable thrust capabilities and how they are being applied to abort systems on launch vehicles and landing rockets for spacecraft. This is the first time that this information will be provided in support of a technical conference.
机译：Aerojet是美国（美国）的领先火箭和太空推进公司，一直在为各种应用开发可控的固体推进剂推进系统，包括生产中的系统。可控固体推进系统通过在操作期间改变喷嘴喉部区域和电动机的操作压力来提供具有高循环比的可变推力能力。 Aerojet开发了许多可控系统，分别具有单个和多个可变推力喷嘴，用于轴向推进火箭电机和姿态控制系统。最近，Aerojet开始在可控推力系统上工作，为机组人员发动车辆和航天器应用，支持NASA的太空勘探计划。本文概述了Aerojet可控推力能力以及如何应用于用于航天器的发动车辆和着陆火箭的中止系统。这是第一次将提供此信息，以支持技术会议。

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