大容量推进剂贮箱液体晃动性能试验

doi:10.3969/j.issn.1674-1579.2016.03.008

Abstract

Abstract: Abstract：Aiming at the bulky propellant tank with propellant management device (PMD), experiment research on liquid sloshing performance is carried out. The liquid sloshing tests in a tank without PMD are developed under different liquid filling ratios. Based on the equivalent mechanical model, the theoretical result of liquid sloshing is calculated. The results of tests and calculation are analyzed and compared. The results are consistent, both the reliability of test system and the validity of theoretical model are well verified. Then the liquid sloshing tests in the tank with PMD are developed under different liquid filling ratios, and the test results indicate that the structure of inner PMD significantly affects the performance of liquid sloshing in the tank. All the experiment research results provide an important reference and data support for designing and optimizing the attitude and orbit control system of rocket and spacecraft.

Key words: Keywords：liquid sloshing, slosh frequency, damping bulky propellant tank, PMD

CLC Number:

HU Qi, LI Yong, YAO Can, LIU Jin-Tao. Experiment of Liquid Sloshing Performance in Bulky Propellant Tank[J]., 2016, 42(3): 44-48.

0
/ / Recommend

Add to citation manager EndNote|Reference Manager|ProCite|BibTeX|RefWorks

URL: http://journal01.magtech.org.cn/Jwk3_kjkzjs/EN/10.3969/j.issn.1674-1579.2016.03.008

http://journal01.magtech.org.cn/Jwk3_kjkzjs/EN/Y2016/V42/I3/44

References

［1］曲广吉.卫星动力学工程［M］.北京:中国科学技术出版社,2000. ［2］杨旦旦,岳宝增.低重环境下旋转轴对称贮箱内液体晃动研究［J］.宇航学报,2013, 34(7): 917-925. YANG D D, YUE B Z. Research on sloshing in axsymmetrical containers under low gravity［J］. Journal of Astronautics, 2013, 34(7): 917-925. ［3］HYUNG R S. Unstructured grid based Reynoldsaveraged navierstokes method for liquid tank sloshing［J］. Journal of Fluid Engineering, Transaction of the ASME, 2005, 127(3): 572-582. ［4］FALTINSEN O M, ROGNEBAKLE O F, TIMOKHA A N. Classification of threedimensional nonlinear sloshing in a squarebase tank with finite depth［J］. Journal of Fluids and Structures, 2005(20): 81-103. ［5］LUPPES R, HELDER J A, VELDMAN A E P. The numerical simulation of liquid sloshing in microgravity［C］//European Conference on Computational Fluid Dynamics. TU Delft, The Netherlands, 2006. ［6］ADLER S, WARSHAVSHY A, PERETZ A. Lowcost coldgas reaction control system for sloshsat FLEVO small satellite［J］. Journal of Spacecraft and Rockets, 2005, 24(2): 345-351. ［7］VELDMAN A E P, GERRITS J, LUPPES R, et al. The numerical simulation of liquid sloshing on board spacecraft［J］. Journal of Computational Physics, 2007, 224: 82-99. ［8］修观,李鑫.火箭三级无动力飞行段晃动的一种建模方法［J］.上海航天, 2015, 32(1): 22-25. XIU G, LI X. A modeling method for propellantsloshing of launch vehicle in third stage flight without power［J］. Aerospace Shanghai, 2015, 32(1): 22-25. ［9］陆国平,李道奎,曾擎.大型平铺贮箱卫星的液体晃动模型与晃动力矩分析［J］.上海航天,2011,28(1):18-22. LU G P, LI D K, ZENG Q. Liquid sloshing model and sloshing torque analysis of large satellite with tiled tank［J］. Aerospace Shanghai, 2011, 28(1): 18-22. ［10］黄华,杨雷,张熇,等.航天器贮箱大幅液体晃动三维质心面等效模型研究［J］.宇航学报,2010, 31(1):55-59. HUANG H, YANG L,ZHANG H， et al. Research on 3D constraint surface model for large amplitude liquid sloshing on spacecraft tank［J］. Journal of Astronautics, 2010, 31(1): 55-59. ［11］林宏,彭慧莲,董锴.推进剂贮箱液体晃动的仿真研究与验证［J］.强度与环境,2011,38(5):25-30. LING H, PENG H L, DONG K. Simulation and test verification for liquid sloshing of propellant tank［J］. Structure & Environment Engineering, 2011, 38(5): 25-30. ［12］李松,高芳清,杨翊仁，等.水平圆柱腔内液体晃动特性试验研究［C］.第14届全国反应堆结构力学会议.北京：中国力学学会，2006. ［13］ABRAMSON H N. The dynamics behavior of liquids in moving containers［R］. NASA SP106, 1996.

[1]	YANG Ling-Zhi, WEI Yan-Ming, LIU Xu-Hui. Development of MEMS Solid Propellant MicroThruster Array [J]. , 2016, 42(1): 13-19.
[2]	HU Qi-Yang, CHEN Jun, LONG Jun, FAN Xu-Feng. The Dynamic Model of Thruster for DragFree Satellite [J]. , 2016, 42(1): 52-56.
[3]	WANG Wei-Chen, SHI Yong, ZHANG Jian, YANG Sheng. On the Process of Orbital Residual Propellant Blowing-off in the Intra-Cavity of Pipeline Connector [J]. , 2014, 40(4): 47-51.
[4]	ZHUANG Bao-Tang, LI Yong, PAN Hai-Lin, HU Qi. Experimental Investigation on FluidStorage Characteristic of Propellant Refillable Reservoir in Microgravity Environment [J]. , 2014, 40(1): 27-30.
[5]	HU Qi, LI Yong, PAN Hai-Lin, LI Ze. Numerical Simulation and Experiment Verification of Fluid Behavior in the Vane Type Tank with Big Vanes in Microgravity Environment [J]. , 2013, 39(2): 58-62.
[6]	ZHUANG Bao-Tang, LI Yong, PAN Hai-Lin, HU Qi, LI Ze. Experiment Investigation on Transportation Velocity of the Fluid on Propellant Acquisition Vanes under Microgravity Environment [J]. , 2012, 38(6): 1-5.
[7]	WANG Feng-Shan, MAO Xiao-Fang, YU Yu-Song, ZHANG Zhen, WANG Ping. Numerical LES Study of Spray Performance in a Bi Propellant Coaxial Centrifugal Injector [J]. , 2012, 38(6): 13-.

Experiment of Liquid Sloshing Performance in Bulky Propellant Tank

PDF (PC)

Like

Knowledge

Abstract

Cite this article

share this article

References

Related Articles 7

Metrics

Comments

Recommended 0