|Table of Contents|

Simulation and analysis of propellant refueling stability under low-gravity condition(PDF)

《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V]

Issue:
2013年04期
Page:
41-45
Research Field:
研究与设计
Publishing date:

Info

Title:
Simulation and analysis of propellant refueling stability under low-gravity condition
Author(s):
LI Le
Shanghai Institute of Space Propulsion, Shanghai 201112, China
Keywords:
low-gravity;  surface tension tank;  propellant refueling;  flow control
PACS:
V434+.23-34
DOI:
-
Abstract:
Based on space refueling technology, the stability of refueling is analyzed in this paper. The FLUENT VOF platform was used to simulate the stability of refueling. The results indicate that the mixture of gas and liquid is easy to appear when propellant refueling is under low-gravity condition, the flow rate should be controlled, or a baffle structure must be adopted in the tank to reduce the liquid momentum at inlet of the tank.

References:

[1]王俊峰, 王月基, 申麟, 等. 上面级多星部署的轨道设计研究[J]. 导弹与航天运载技术, 2011, 31(1): 7-9.
[2]刘国球. 液体火箭发动机原理[M]. 北京: 中国宇航出版社, 1993.
[3]朱宁昌. 液体火箭发动机设计[M]. 北京: 中国宇航出版社, 1993.
[4]杨世铭, 陶文铨. 传热学[M]. 3版. 北京: 高等教育出版社, 2002.
[5]WANG Ten-See, LIN Jeff, RUF Joe, et al. Effect of coolant flow distribution on transient side load of film cooled nozzles, AIAA 2011-3268 [R]. USA: AIAA, 2011.
[6]REIJASSE Philippe, BOCCALETTO Luca. Influence of film cooling on nozzle side load, AIAA 2008-392 [R]. USA: AIAA, 2008.
[7]REIJASSE Philippe, BOCCALETTO Luca. Nozzle flow control with a wall film injection, AIAA 2007-5747 [R]. USA: AIAA, 2007.
[8]REIJASSE Philippe, BOCCALETTO Luca. Nozzle flow separation with film cooling, AIAA 2008-4150 [R]. USA: AIAA, 2008.
[9]PERROT Y, HADJADJ A. Numerical simulation of shock boundary layer interaction in supersonic nozzles, AIAA 2005-4309 [R]. USA: AIAA, 2005.
[10]PERROT Y, HADJADJ A. Shock pattern in the plume of rocket nozzles needs for design consideration, AIAA 2005-4309 [R]. USA: AIAA, 2005.
[11]BOCCALETTO L, CAHUZAC F. Solving the flow separation issue a new nozzle concept, AIAA 2008-5234 [R]. USA: AIAA, 2008.
[12]WANG Ten-See, LIN Jeff, RUF Joe. Transient three-dimensional side-load analysis of out-of-round film-cooled nozzles [J]. Journal of Propulsion and Power, 2011, 27(4): 899-907.
[13]FERRANDON O, JAMES P H, GIRARD P H. Vulcain 2 nozzle extension integrated European team and advanced computational models to the service of nozzle design, AIAA 2005-4535 [R]. USA: AIAA, 2005.

Memo

Memo:
-
Last Update: 1900-01-01