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1.引言最近几年,对发展探纵战术导弹的新方法已经给了很多注意。特别重要的一种方法即大家已知的推力矢量控制,它以推进发动机的排气流的矢量来操纵导弹。在液体燃料发动机的场合,通常的推力矢量技术是转动整个燃烧室。但这种方法对于固体推进发动机不适用,因此提出了另外的技术。这篇介绍论文就各种系统作了比较,这些系统新近在英国开始发展,现已可供设计应用。
1. INTRODUCTION In recent years, much attention has been given to the development of new methods for the exploration of tactical missiles. One particularly important method is known as thrust vector control, which steers the missile with a vector that advances the exhaust flow of the engine. In the case of liquid fuel engines, the usual thrust vectoring technique is to turn the entire combustion chamber. However, this method is not suitable for solid propellant engines and therefore proposes another technique. This introductory paper compares various systems that were recently developed in the UK and are now available for design and application.