本論文的主旨為研發一個應用於太空環境的推進劑燃料槽。此燃料槽設計主要包括兩大主體結構部分，分別為圓筒型燃料槽體及內部活塞與密封配件，吾人利用有限元素商業軟體ANSYS來探討密封環的接觸問題，並考慮模型中密封環與槽體不同的接觸型式以確保實體結構之密封性。本文針對燃料槽結構進行靜態與動態分析，並考慮適當的環境測試規格以確保燃料槽在太空中能有效運作。為了確保分析模型的有效性，本研究亦進行實驗模態分析，並藉由與試驗結果的比較來修正模型。

The purpose of this thesis is to develop a propellant fuel tank which can be applied to space environment. The design of this fuel tank is mainly divided into two major structural parts which are cylindrical fuel tank and internal piston/seal accessory. The commercial ANSYS finite element analysis software is used to explore the contact problem of seal ring. We also consider different models of contact between seal ring and tank to ensure the tightness of physical structure. This article focuses on performing static and dynamic analysis on the structure of fuel tank. An appropriate testing environment level is also considered to assure that fuel tank can be effectively operated. We also conduct modal analysis and confirm the model validity by comparing with the testing result.

[1]I. A. Ballinger, W. D. Lay, and W. H. Tam, "Review and
History of PSI Elastomeric Diaphragm Tanks ", 31st
AIAA/ASME/SAE/ASEE Joint Propulsion Conference and
Exhibit, Paper No.: AIAA95-2534, San Diego, CA., 10-12
July, 1995.

[2]M. J. Debreceni, W. D. Lay, D. E. Jaekle and A. C.
Graffer, "Design & Development of the AXAF-IPS PMD & PMD
Integration", 33rd AIAA/ASME/SAE/ASEE Joint Propulsion
Conference and Exhibit, Paper No.: AIAA97-2812, Seattle,
WA., 6-9 July, 1997.

[3]Walter H. Tam, Jerry Kuo and Don E. Jaekle, "Design and
Manufacture of an Ultra-lightweight Propellant Management
Device", 44rd AIAA/ASME/SAE/ASEE Joint Propulsion
Conference and Exhibit, Paper No.: AIAA 2002-4137, 2002.

[4]唐紹文,“低推力聯安推進系統之設計與不穩定特性分析”, 國立成功大學航空太
空工程研究所碩士論文,2008.

[5]J.-J. Miau and J. C. Juang, “A university nano-satellite
program: PACESAT,” 5th IAA Symposium on Small Satellites
for Earth Observation, IAA-B5-0 510P, Berlin, Germany, 4-
8 April, 2005.

[6]國家太空中心,“福爾摩沙5組件環境規範”,: Version FS5-SPEC-0003,
2010.

[7]“ISL.ISILaunch.EL.PSLV - Environment Levels,” V. 1.4,
ISILaunch Services, 2010.

[8]Basem Alzahabi and Logesh Kumar, "Natarajan Correlation
of Modal Characteristics of Circular Cylindrical Shells",
C. S. Mott Engineering and Science Center Department of
Mechanical Engineering Kettering University 1700 West
Third Avenue Flint, Michigan, 48504, USA.
[9]He, J., & Fu, Z.-F., "Modal Analysis," 2001.

[10]McConnell, K. G., "Vibration Testing: Theory and
Practice", John Wiley & Sons, Inc. New York, 1995.

[11]王栢村，「實驗模態分析」，屏東科技大學課程講義，2000。

[12]王栢村，陳榮亮，「頻譜分析儀之功能測試」，中華民國振動與噪音工程學會
第九屆學術研討會論文集，第16-20頁，2001。

[13]Ewins, D. J., "Modal Testing: Theory and Practice",
Research Studies Press Ltd., Letchworth, Hertfordshire,
England, 1986.

[14]Ho, B. L. and Kalman, R. E., “Effective Construction of
Linear State-Variable Models from Input/Output Data”,
Proceedings of the 3rd Annual Allerton Conference on
Circuit and System Theory, pp. 449-459, 1965.

[15]Zeiger, H. P. and McEwen, A. J., “Approximate Linear
Realizations of Given Dimension Via Ho’s Algorithm”,
IEEE Transactions on Automatic Control, Vol. AC-19, No.
2, pp. 153-153, 1974.

[16]Juang, J. N. and Pappa, R. S., “An Eigensystem
Realization Algorithm for Modal Parameter Identification
and Model Reduction”, Journal of Guidance, Control and
Dynamics, Vol. 8, No. 5, pp. 620-627, 1985.

[17]Juang, J. N., Cooper, J. E. and Wright J. R., “An
Eigensystem Realization Algorithm using Data
Correlations (ERA/DC) for Modal Parameter
Identification”, Control-Theory and Advanced Technology,
Vol. 4, No. 1, pp. 5-14, 1988.

[18]Pappa, R. S. and Ibrahim, S. R., “A Parametric Study of
Ibrahim Time Domain Modal Analysis”, Shock and Vibration
Bulletin, Vol. 51, Part. 3, pp. 43-72, 1981.

[19]Vold, H. and Rocklin, G. F., “The Numerical
Implementation of a Multi-Input Modal Estimation Method
for Mini- Computers”, International Modal Analysis
Conference Proceedings, 1982.

[20]Basem Alzahabi and Logesh Kumar " Natarajan Correlation
of Modal Characteristics of Circular Cylindrical Shells
" C. S. Mott Engineering and Science Center Department
of Mechanical Engineering Kettering University 1700 West
Third Avenue Flint, Michigan, 48504, USA

[21]Wang Jie and Xie Yu-jun, "Ansys Analysis of Rubber O -
Sealing Ring", Journal of Liaoning University of
Petroleum & Chemical Technology, Vol. 28, No. 4, pp. 48-
50, 2008.

[22]黃源聖,“奈米級衛星軌道彈射艙減振設計與分析”, 國立成功大學航空太空工
程研究所碩士論文, 2012.