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辐射式金属空楔结构PMD元件的设计基础
引用本文:张天平,程彬.辐射式金属空楔结构PMD元件的设计基础[J].上海航天,1999,16(6):9-14.
作者姓名:张天平  程彬
作者单位:兰州物理研究所!兰州730000
摘    要:在长寿命卫星表面张力贮箱技术的发展中,孔板式推进剂管理装置(PMD)正在逐渐取代传统的筛网式PMD,而辐射式金属空楔结构是孔板式PMD中的最重要元件之一。主经介绍了讨论了辐射式金属空楔结构PMD元件设计中的基本问题,包括蓄留体积设计、蓄留能力设计和空楔结构性能分析等方面的主要内容,并给出了详细分析金属楔结构元件性能的一个具体设计实例。

关 键 词:辐射式空楔结构  推进剂管理装置  贮箱  设计  PMD

THE DESIGN ESSENCE OF A RADIAL SPONGE
ZHANG Tian ping,CHENG Bin,CHEN Meng jun.THE DESIGN ESSENCE OF A RADIAL SPONGE[J].Aerospace Shanghai,1999,16(6):9-14.
Authors:ZHANG Tian ping  CHENG Bin  CHEN Meng jun
Abstract:The traditional screen based propellant management device (PMD) is replaced gradually by the perforated sheet based PMD with the technique progress in the surface tension tank of a long life satellite. A radial sponge is one of the most important component of the perforated sheet based PMD. In this paper, the physical design essences of a radial sponge, mainly including its volume design, its retaining capability design and the analysis of its performance, are introduced and discussed briefly. At last, an example design of a radial sponge is presented and its performance is analyzed in detail.
Keywords:Radial sponge  Propellant management device  Tank  Design  Performance analysis
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