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[1]宁继荣,陈祖奎,马 键,等.可再充填启动篮表面张力推进剂管理装置设计及试验研究[J].火箭推进,2011,37(02):25-29.
　NING Ji-rong,CHEN Zu-kui,MA Jian,et al.Design and test of refillable start-basket surface tension PMD[J].Journal of Rocket Propulsion,2011,37(02):25-29.
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可再充填启动篮表面张力推进剂管理装置设计及试验研究

《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V] 卷: 37 期数: 2011年02期 页码: 25-29 栏目: 研究与设计 出版日期: 2011-04-15
Title:
Design and test of refillable start-basket surface tension PMD
文章编号:
1672-9374(2011)02-0038-05
作者:
宁继荣; 陈祖奎; 马 键; 穆小强
西安航天动力研究所，陕西 西安 710100
Author(s):
NING Ji-rong;  CHEN Zu-kui;  MA Jian;  MU Xiao-qiang
Xi’an Aerospace Propulsion Institute, Xi’an 710100, China
关键词:
可再充填启动篮; 推进剂管理装置; 设计; 分析
分类号:
V511-34
文献标志码:
A
摘要:
对启动篮表面张力推进剂管理装置工作原理进行了说明，建立了可再充填启动篮再充填过程仿真模型，根据仿真结果对影响启动篮再充填的各种因素进行了分析。加工原理性试验件进行了静态充填试验和动态充填试验，试验结果和仿真结果基本一致，验证了计算模型的正确性。初步掌握了可再充填启动篮表面张力推进剂管理装置设计、加工和地面试验技术。
Abstract:
The working principle of the start-basket surface tension PMD is described. A simulation model of the refilling process of the refillable start-basket is established and the factors which affect the refilling process are analyzed. A test sample was manufactured, and then the static and dynamic refilling tests were carried out. The test results have a good agreement with the simulation tests, which indicates the validity of the simulation model. The design, manufacture and test technology of the refillable start-basket have been mastered preliminarily. The design is important to develop the tank used in restartable propulsion system.

参考文献/References:

[1]JAEKLE D E，Jr. Propellant management device conceptual design and analysis: traps and troughs, AIAA 95-2531 [R]. USA : AIAA, 1995.
[2]ROLLINS J R， GROVE R K， JAEKLE D E, Jr. Twenty three years of surface tension propellant management system design，development manufacture test and operation, AIAA 85-1199[R]. USA: AIAA, 1985.
[3]BLATT M H, MERINO Fred, SYMONS E Patrick. Capillary device refilling. AIAA 80-1095[R]. USA: AIAA, 1980.
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[6]GAINES R D, ORTIN G F. Recent development in propellant acquisition technology, AIAA 84-1477[R]. USA: AIAA, 1984.
[7]CHAPTER J J, RIDER S B. Surface tension propellant management system computerized flow analysis, AIAA-80-1098[R]. USA: AIAA, 1980.
[8]HEUREUX J M Computational solution for the free surface in a propellant tank, AIAA 87-2020[R]. USA: AIAA, 1987.

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备注/Memo

收稿日期：2010-11-13；修回日期：2010-12-22
作者简介： 宁继荣（1980—），男，工程师，研究领域为液体火箭推进系统总装设计

更新日期/Last Update: 1900-01-01