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PROPULSION MODULE FOR RENDEZ-VOUS DOCKING

机译:Rendez-Vous对接的推进模块

摘要

PURPOSE:To enable exchange of a propulsion system only by disposing thrusters having thrust vectors which are inclined from the surface outward at a suitable angle and turned to four directions intersecting each other at right angles at four designated positions where two portions on the forward wide are opposite to each other and two portions on the rear side are opposite to each other. CONSTITUTION:The progress direction of a space flying main body 1 is left (+ x axis direction) in the vertical direction in the drawing, and a propulsion module 2 is fitted to the terminal portion of the flying main body 1. Thruster clusters (thruster will be satisfactory) 3-6 are disposed at positions on the upper surface and the lower surface of the propulsion module 2 in the vertical direction in the drawing, that are symmetrical to the front portion and the rear portion. The respective thruster clusters are inclined from the arrangement surface outwards at a suitable angle and have thrust vectors turned to four directions (C11-C14, C21-C24, C31-C34, C41-C44) intersecting each other at right angles. These are combined to control jet of the respective thruster clusters 3-6 so that translation force in the directions of three axes and turning torque round these axes can be independently generated.
机译:目的:仅通过将推力矢量布置在推力矢量上,以实现推进系统的更换,推力矢量从表面向外倾斜适当的角度,并在四个指定位置(彼此相交成直角的四个方向)相交,前向宽度上的两个部分分别为彼此相对,并且后侧的两个部分彼此相对。组成:太空飞行主体1的前进方向在图中的垂直方向上为左(+ x轴方向),并且推进模块2安装在飞行主体1的终端部分。 3-6布置在推进模块2的沿图的竖直方向上的上表面和下表面上的位置,该位置与前部和后部对称。各个推进器簇从布置表面向外以合适的角度倾斜,并且具有朝向彼此正交的四个方向(C11-C14,C21-C24,C31-C34,C41-C44)的推力矢量。这些被组合以控制各个推进器组3-6的射流,从而可以独立地产生在三个轴的方向上的平移力以及围绕这些轴的转动转矩。

著录项

  • 公开/公告号JPH01245000A

    专利类型

  • 公开/公告日1989-09-29

    原文格式PDF

  • 申请/专利权人 NEC CORP;

    申请/专利号JP19880071126

  • 发明设计人 AOYAMA JUNICHI;

    申请日1988-03-25

  • 分类号B64G1/64;

  • 国家 JP

  • 入库时间 2022-08-22 06:44:48

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