航天推进技术研究院主办
ZHANG Yu-hua.Equalizing expulsion and control of parallel tanks in propulsion system[J].Journal of Rocket Propulsion,2013,39(03):83-86.
推进系统并联贮箱均衡排放性能及其控制措施
- Title:
- Equalizing expulsion and control of parallel tanks in propulsion system
- 文章编号:
- 1672-9374(2013)03-0067-05
- Keywords:
- metallic diaphragm tank; propulsion system; equalizing expulsion; con
- 分类号:
- V434-34
- 文献标志码:
- A
- 摘要:
- 推进系统在工作过程中,贮箱排放的不均衡性将引起飞行器质心偏移,产生干扰力矩。对空间推进系统并联工作的金属膜片贮箱均衡排放的影响因素进行了分析,结合均衡排放的控制措施对某型号推进系统工作过程中的排放不均衡量进行了预计,并与飞行试验结果进行了比对。飞行试验结果表明控制措施可行、有效。
- Abstract:
- The propellant tank is an important component of the space propulsion system. During the operation of the propulsion system, the unequal expulsion of the metallic diaphragm tanks will lead to the variation of the spacecraft centroid, which will result in interference moment. The factors which affect the equal expulsion of parallel metallic diaphragm tanks in the propulsion system are analysed. The unequal expulsion degree of a propulsion system is estimated in combination with the measures of controlling the expulsion. It is compared with the results of flight experiment. The results show that the control measure is feasible and effective.
相似文献/References:
[1]曹 伟,王 睿,陈 剑,等.推进剂管路内负压形成机理研究[J].火箭推进,2015,41(04):37.
CAO Wei,WANG Rui,CHEN Jian,et al.Research on formation mechanism of negative pressure phenomenon in propellant pipeline[J].Journal of Rocket Propulsion,2015,41(03):37.
[2]陈阳春,王爱华,汤建华.某发动机喷管周围流场研究[J].火箭推进,2013,39(05):41.
CHEN Yang-chun,WANG Ai-hua,TANG Jian-hua.Research of flow field around nozzle of an engine[J].Journal of Rocket Propulsion,2013,39(03):41.
[3]袁 磊,王 申,连仁志,等.一种推进剂剩余量在轨测量方法研究[J].火箭推进,2013,39(05):75.
YUAN Lei,WANG Shen,LIAN Ren-zhi,et al.On-board gauging method of remaining propellant[J].Journal of Rocket Propulsion,2013,39(03):75.
[4]刘 川,刘 俊,邱 鑫,等.火星探测器推进系统初步设想[J].火箭推进,2014,40(02):44.
LIU Chuan,LIU Jun,QIU Xin,et al.Preliminary design of propulsion system
for Mars exploration[J].Journal of Rocket Propulsion,2014,40(03):44.
[5]魏彦祥,赵 京.用于并联金属膜片贮箱均衡排放的一种控制方法[J].火箭推进,2012,38(05):37.
WEI Yan-xiang,ZHAO Jing.Control method for equal expulsion of parallel metallic diaphragm tanks[J].Journal of Rocket Propulsion,2012,38(03):37.
[6]张增亭.金属膜片贮箱膜片的数值仿真与试验验证[J].火箭推进,2009,35(03):26.
Zhang Zengting.Numerical simulation and test veritication ot
diaphragm for metal diaphragm tank[J].Journal of Rocket Propulsion,2009,35(03):26.
[7]陈朝,黄敏超.空间轨道转移飞行器推进系统静态仿真分析[J].火箭推进,2007,33(06):22.
Chen Zhao,Huang Minchao.Static state simulation study of orbital transfer vehicle propulsion system[J].Journal of Rocket Propulsion,2007,33(03):22.
[8]戴佳,黄敏超,沈赤兵,等.双组元液体挤压推进系统启动过程时序分析[J].火箭推进,2006,32(02):16.
Dai Jia,Huang Minchao,Shen Chibing,et al.Startup process timing analysis of liquid bipropellant pressure-fed propulsion system[J].Journal of Rocket Propulsion,2006,32(03):16.
[9]丁丰年,张恩昭,张小平,等.论我国重复使用运载器推进系统方案[J].火箭推进,2004,(03):13.
[10]刘昌波.电动泵与挤压式推进系统对比研究[J].火箭推进,2017,43(02):32.
LIU Changbo.Comparative study on electric pump and pressure-fed propulsion systems[J].Journal of Rocket Propulsion,2017,43(03):32.
[11]刘锋,周进.金属膜片贮箱推进剂消耗不平衡分析[J].火箭推进,2006,32(05):28.
Liu Feng,Zhou Jin.Analysis of the unbalanced depletion of the propellant for the metal diaphragm tank[J].Journal of Rocket Propulsion,2006,32(03):28.
备注/Memo
收稿日期:2012-07-12;修回日期:2012-12-04
基金项目:中国航天科技集团公司支撑项目(2009JY06)
作者简介:章玉华(1971—),女,高级工程师,研究领域为空间推进系统设计