Abstract
Space Launch Vehicle (SLV) is a system to transport and place the Payloads (PL) such as satellites, experimental tools, and observation robots into desired orbit. PL are transported in Payload Fairing (PLF) that is a part of SLV and protects PL from environmental effects exposed during SLV’s flight. PL capacity is the major criteria in design of SLVs. One option to increase PL capacity of SLV is to minimize PLF weight while protecting the volume allocated for PL. In this study, an Optimization System (OS) is developed to minimize PLF weight while maintaining the PLF structural design strong enough to protect PL from effects such as aerodynamic and inertial loads that emerged from flight conditions. Tabu Search is integrated to the OS to perform optimization. Structural analysis program is integrated to the OS to evaluate the structural strength. It is found that an optimized and structurally appropriate PLF configuration can be selected with Tabu Search integrated OS.
References
- [1] Krivanek T.M., Yount B.C. (2012), Composite Payload Fairing Structural Architecture Assessment and Selection, E-18094, NASA Glenn Research Center, Cleveland. [2] Wenger P.M., Higgins J. E., VanWest B. P. (2002) Application of Advanced Grid-Stiffened Structures Technology to the Minotaur Payload Fairing, AIAA 2002-1336, 1061-1067. [3] Irish Angelin S., Senthilkumar S. (2013) Aerodynamic Shaping of Payload Fairing for Launch Vehicle, Journal of Spacecraft and Rockets, Vol. 50, No. 6, pp. 1299-1304. doi: 10.2514/1.A32838. [4] Reisenthel P. H. ,Childs R. E., Higgins J. E., (2007) Surrogate-Based Design Optimization of a Large Asymetric Launch Vehicle Payload Fairing, 46th Aerospace Sciences Meeting and Exhibit, 2007-0361, ISSN: 10877215 [5] Togan V., Seyhun M. O., Daloglu A. (2015) A Comparative Study For The Optimum Design of StructuresUsing GeneticAlgorithm, www.researchgate.bet, search on 15th of June. [6] Kargahi, M. and Anderson, J. (2006) Structural Weight Optimization with Tabu Search. Earth & Space 2006: pp. 1-8. doi: 10.1061/40830(188)163. [7] Connor, A.M., Seffen, K.A., Clarkson, P.J. & Parks, G.T. (1999) Efficient Optimisation Of Structures Using Tabu Search, Proceedings of the 1st ASMO/ISSMO Conference on Engineering Design Optimization, 127-134 [8] A. Gauchía, B.L. Boada, M.J.L. Boada and V. Díaz (2014). Integration of MATLAB and ANSYS for Advanced Analysis of Vehicle Structures, MATLAB Applications for the Practical Engineer, Mr Kelly Bennett (Ed.), ISBN: 978-953-51-1719-3 [9] Zafar N., Linshu H., (2010) Multidisciplinary Design Optimization of Solid Launch Vehicle Using Hybrid Algorithm, 51st AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, andMaterials Conference, DOI: 10.2514/6.2010-3010 [10] Inc. PADT, Strain J.,“Introduction to the ANSYS Parametric Design Language (APDL): A Guide to the ANSYS Parametric Design”, CreateSpace Independent Publishing Platform; 1 edition, ISSN: 146641135X [11] Bayley D. J., Hartfield R J., Burkhalter J E., , Jenkins R M.(2008), Design Optimization of a Space Launch Vehicle Using a Genetic Algorithm, Journal of Spacecraftand Rockets, Vol. 45, No. 4 , pp. 733-740.doi: 10.2514/1.35318.
Abstract
References
- [1] Krivanek T.M., Yount B.C. (2012), Composite Payload Fairing Structural Architecture Assessment and Selection, E-18094, NASA Glenn Research Center, Cleveland. [2] Wenger P.M., Higgins J. E., VanWest B. P. (2002) Application of Advanced Grid-Stiffened Structures Technology to the Minotaur Payload Fairing, AIAA 2002-1336, 1061-1067. [3] Irish Angelin S., Senthilkumar S. (2013) Aerodynamic Shaping of Payload Fairing for Launch Vehicle, Journal of Spacecraft and Rockets, Vol. 50, No. 6, pp. 1299-1304. doi: 10.2514/1.A32838. [4] Reisenthel P. H. ,Childs R. E., Higgins J. E., (2007) Surrogate-Based Design Optimization of a Large Asymetric Launch Vehicle Payload Fairing, 46th Aerospace Sciences Meeting and Exhibit, 2007-0361, ISSN: 10877215 [5] Togan V., Seyhun M. O., Daloglu A. (2015) A Comparative Study For The Optimum Design of StructuresUsing GeneticAlgorithm, www.researchgate.bet, search on 15th of June. [6] Kargahi, M. and Anderson, J. (2006) Structural Weight Optimization with Tabu Search. Earth & Space 2006: pp. 1-8. doi: 10.1061/40830(188)163. [7] Connor, A.M., Seffen, K.A., Clarkson, P.J. & Parks, G.T. (1999) Efficient Optimisation Of Structures Using Tabu Search, Proceedings of the 1st ASMO/ISSMO Conference on Engineering Design Optimization, 127-134 [8] A. Gauchía, B.L. Boada, M.J.L. Boada and V. Díaz (2014). Integration of MATLAB and ANSYS for Advanced Analysis of Vehicle Structures, MATLAB Applications for the Practical Engineer, Mr Kelly Bennett (Ed.), ISBN: 978-953-51-1719-3 [9] Zafar N., Linshu H., (2010) Multidisciplinary Design Optimization of Solid Launch Vehicle Using Hybrid Algorithm, 51st AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, andMaterials Conference, DOI: 10.2514/6.2010-3010 [10] Inc. PADT, Strain J.,“Introduction to the ANSYS Parametric Design Language (APDL): A Guide to the ANSYS Parametric Design”, CreateSpace Independent Publishing Platform; 1 edition, ISSN: 146641135X [11] Bayley D. J., Hartfield R J., Burkhalter J E., , Jenkins R M.(2008), Design Optimization of a Space Launch Vehicle Using a Genetic Algorithm, Journal of Spacecraftand Rockets, Vol. 45, No. 4 , pp. 733-740.doi: 10.2514/1.35318.
Details
| Primary Language | English |
|---|---|
| Subjects | Engineering |
| Journal Section | Araştırma Articlessi |
| Authors | |
| Publication Date | December 30, 2015 |
| Published in Issue | Year 2015 Volume: 3 |
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