Advanced Strategic Planning and Capability Identification in Order to Develop a Liquid Hydrogen Turbopump

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This paper presents the activities that define a strategic development plan for a new liquid hydrogen turbopump that will equip a rocket engine and the capabilities of COMOTI Romanian Research and Development Institute for Gas Turbines in order to develop such type of product. The paper highlights the design, assembly and manufacturing stages for the two main components of a turbopump, the pump and the turbine. Subjected to analysis are the constructive solutions, performances, software for hydraulic, gasodynamic and stress calculus, and also the manufacturing technologies.

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66-71

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June 2014

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© 2014 Trans Tech Publications Ltd. All Rights Reserved

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[1] Caissoa P. et al., A Liquid Propulsion Panorama, Acta Astronautica, vol. 65, 2009, pp.1723-1737.

Google Scholar

[2] Alliot P, Dalbies, E, Delange, J-F, Ruault, J-M, Development status of the VINCI engine for the Ariane 5 Upper Stage, AIAA 2003-4484, 2003, Austin, U.S.A. - 9.

DOI: 10.2514/6.2003-4484

Google Scholar

[3] Brodin S., J. Steen, I. Ljungkrona, N. Edin, B. Laumert, Vinci Engine Development Testing, A Summary of Turbine Testing Results, AIAA-2005-3949, 2005, San Francisco, U.S.A. -10.

DOI: 10.2514/6.2005-3949

Google Scholar

[4] B. Lakshminarayana, An assessment of computational fluid dynamic techniques in the analysis and design of turbomachinery, ASME Journal of Fluids Engineering, vol. 113, pp.315-352, (1991).

DOI: 10.1115/1.2909503

Google Scholar

[5] S. Thakur, J. Wright, W. Shyy, J. Liu, H. Ouyang, and T. Vu, Development of pressure-based composite multigrid methods for complex fluid flows, Program in Aerospace Science, vol. 32, pp.313-375, (1996).

DOI: 10.1016/0376-0421(95)00008-9

Google Scholar

[6] Tuzson J. – Centrifugal Pump Design, 2000, John Wiley & Sons.

Google Scholar

[7] J. Popescu, R. Mihalache, V. Vilag Determining the Flue Gases Composition At The Inlet of the Turbine Section For a Rocket Turbopump 1st International Conference New Challenges in Aerospace Sciences NCAS 2013, pp.162-165.

Google Scholar

[8] V. Silivestru, R. Mihalache, C. Silivestru, J. Popescu, V. Stanciu Advanced Strategic Planning Regarding the Development of a Turbopump System for a Liquid Fuel Rocket Engine The CEAS European Air & Space Conference 2013, 16-19 Sept. 2013, Linköping University, Sweden Available online from: http: /www. ceas2013. org/images/images/CEAS2013. pdf.

Google Scholar

[9] David Japikse & Nicholas C. Baines - Introduction to Turbomachinery, Concepts ETI, Inc. And Oxford University Press, Vermont, USA, 1994, ISBN: 0-933283-10-5.

Google Scholar

[10] Stanciu, V. & Rotaru, E., "Teoria Sistemelor de Propulsie Aeriene , Editura Bren, Bucureşti, Romania, 2003, ISBN 973-648 -127-1.

Google Scholar

[11] Stanciu, V., Miclescu, A. & Mogos, G., Aplicaţii ale teoriei sistemelor de propulsie aeriene, Editura Printech, Bucureşti, 2005, ISBN 973-718- 167-0.

Google Scholar

[12] Pimsner, V., Teoria si constructia sistemelor de propulsie, Institutul Politehnic Bucureşti, (1984).

Google Scholar

[13] Cuciumita Cleopatra, Radu Mihalache, Daniel Olaru, Jeni Popescu, Valeriu Vilag Design of a Liquid Hydrogen Turbine to Drive a Rocket Engine Turbopump 1st International Conference New Challenges in Aerospace Sciences NCAS 2013, pp.162-165.

DOI: 10.4028/www.scientific.net/amm.555.66

Google Scholar