How to cite this paper
Aborehab, A., Kassem, M., Nemnem, A., Kamel, M & Kamel, H. (2020). Configuration design and modeling of an efficient small satellite structure.Engineering Solid Mechanics, 8(1), 7-20.
Refrences
Abdelal, G. F., Abuelfoutouh, N., & Gad, A. H. (2013). Finite Element Analysis for Satellite Structures. Springer.
Abdelal, G. F., Abuelfoutouh, N., & Hamdy, A. (2008). Mechanical fatigue and spectrum analysis of small-satellite structure. International Journal of Mechanics and Materials in Design , 4 (3), 265-278.
Ampatzoglou, A., & Kostopoulos, V. (2018). Design, Analysis, Optimization, Manufacturing, and Testing of a 2U Cubesat. International Journal of Aerospace Engineering .
Bai, Z., Zhao, Y., Ma, W., & Tian, H. (2008). Modal Analysis for Small Satellite System with Finite Element Method. International Symposium on Systems and Control in Aerospace and Astronautics. Shenzhen.
Bianchi, G., Aglietti, G. S., & Richardson, G. (2010). Development of Efficient and Cost-Effective Spacecraft Structures Based on Honeycomb Panel Assemblies. IEEE Aerospace Conference.
Byun, W., Kim, M., Park, K., Kim, S., Chung, M., Cho, J., et al. (2013). Buckling analysis and optimal structural design of supercavitating vehicles using finite element technology. International Journal of Naval Architecture and Ocean Engineering , 3, 274-285.
Caprioli, D. (2008). FE simulation of honeycomb core sandwich panels for the body. ATZ worldwide , 110, 26-30.
Catapano, A., & Montemurro, M. (2014). Optimal design of sandwich plates with honeycomb core. Joint Conference on Mechanical, Design Engineering & Advanced Manufacturing (pp. pp.1-7). France: Springer Verlag.
DNEPR. ( 2001). DNEPR space launch system user's guide. Moscow: ISC Kosmotras.
Gibson, L., & Ashby, M. (1997). Cellular Solids : Structure and Properties, 2nd edition. Cambridge: Cambridge University Press.
Hao, L., Geng, L., Shangjun, M., & Wenbin, L. (2011). Dynamic Analysis of the Spacecraft Structure on Orbit Made up of Honeycomb Sandwich Plates. IEEE International Conference on Computer Science and Automation Engineering . Shanghai.
HEXCEL-Composites. (1999). HexWeb Honeycomb Attributes and Properties. Hexcel Composites.
Israr, A. (2014). Vibration and Modal Analysis of Low Earth Orbit Satellite. Shock and Vibration , 2014.
Jiang, D., Zhang, D., Fei, Q., & Wu, S. (2014). An approach on identification of equivalent properties of honeycomb core using experimental modal data. Finite Elements in Analysis and Design, 90, 84–92.
Kim, B., & Lee, D. L. (2010). Development of a satellite structure with the sandwich T-joint. Composite Structures , 460–468.
Kuo, J.-C., Chou, C.-W., Chang, C.-P., & Hung, H.-C. (2017). FORMOSAT-5 satellite Structure Development and Dynamic Launch Environment Verification. 68th International Astronautical Congress (IAC). Adelaide, Australia.
Li, D., Wang, R., Qian, R., Liu, Y., & Qing, G. (2016). Static response and free vibration analysis of the composite sandwich structures with multi-layer cores. International Journal of Mechanical Sciences , 101-115.
Maythraza, M., Anitha, D., Dash, P. K., & Kumar, P. R. (2018). Vibration analysis of honeycomb sandwich panel in spacecraft structure. International Journal of Mechanical and Production Engineering Research and Development, 8(3), 849-860.
Ontac, S., Dag, S., & Gokler, M. (2007). Structural Finite Element Analysis of stiffened and honey comb panels of RASAT satellite. 3rd International IEEE Conference on Recent Advances in Space Technologies.
Rice, R. C., Jackson, J. L., Bakuckas, J., & Thompson, S. (2003). Metallic Materials Properties Development and Standardization. Washington, D.C.: Office of Aviation Research.
Safarabadi, M., & Bazargan, S. (2015). Prediction of equivalent static loads act on a micro satellite via modal analysis. Engineering Solid Mechanics, 3(2), 75-84.
Sairajan, K., & Nair, P. (2010). Design of low mass dimensionally stable composite base structure for a spacecraft. Journal of Composites: Part B , 280-288.
Sun, W. Q., & Cheng, W. (2017). Finite element model updating of honeycomb sandwich plates using a response surface model and global optimization technique. Structural and Multidisciplinary Optimization, 55(1), 121-139.
Wagih, A., Hegaze, M. M., & Kamel, M. A. (2016). Pre-testing Analysis of large remote sensing satellite’s structure. AIAA SPACE 2016. Long Beach, California, USA.
Zheng, K., Liao, W. H., & Qin, Y. T. (2010). Analysis and Research of Honeycomb Sandwich structure for microsatellite based on equivalent theory. In Key Engineering Materials (Vol. 426, pp. 472-476). Trans Tech Publications.
Abdelal, G. F., Abuelfoutouh, N., & Hamdy, A. (2008). Mechanical fatigue and spectrum analysis of small-satellite structure. International Journal of Mechanics and Materials in Design , 4 (3), 265-278.
Ampatzoglou, A., & Kostopoulos, V. (2018). Design, Analysis, Optimization, Manufacturing, and Testing of a 2U Cubesat. International Journal of Aerospace Engineering .
Bai, Z., Zhao, Y., Ma, W., & Tian, H. (2008). Modal Analysis for Small Satellite System with Finite Element Method. International Symposium on Systems and Control in Aerospace and Astronautics. Shenzhen.
Bianchi, G., Aglietti, G. S., & Richardson, G. (2010). Development of Efficient and Cost-Effective Spacecraft Structures Based on Honeycomb Panel Assemblies. IEEE Aerospace Conference.
Byun, W., Kim, M., Park, K., Kim, S., Chung, M., Cho, J., et al. (2013). Buckling analysis and optimal structural design of supercavitating vehicles using finite element technology. International Journal of Naval Architecture and Ocean Engineering , 3, 274-285.
Caprioli, D. (2008). FE simulation of honeycomb core sandwich panels for the body. ATZ worldwide , 110, 26-30.
Catapano, A., & Montemurro, M. (2014). Optimal design of sandwich plates with honeycomb core. Joint Conference on Mechanical, Design Engineering & Advanced Manufacturing (pp. pp.1-7). France: Springer Verlag.
DNEPR. ( 2001). DNEPR space launch system user's guide. Moscow: ISC Kosmotras.
Gibson, L., & Ashby, M. (1997). Cellular Solids : Structure and Properties, 2nd edition. Cambridge: Cambridge University Press.
Hao, L., Geng, L., Shangjun, M., & Wenbin, L. (2011). Dynamic Analysis of the Spacecraft Structure on Orbit Made up of Honeycomb Sandwich Plates. IEEE International Conference on Computer Science and Automation Engineering . Shanghai.
HEXCEL-Composites. (1999). HexWeb Honeycomb Attributes and Properties. Hexcel Composites.
Israr, A. (2014). Vibration and Modal Analysis of Low Earth Orbit Satellite. Shock and Vibration , 2014.
Jiang, D., Zhang, D., Fei, Q., & Wu, S. (2014). An approach on identification of equivalent properties of honeycomb core using experimental modal data. Finite Elements in Analysis and Design, 90, 84–92.
Kim, B., & Lee, D. L. (2010). Development of a satellite structure with the sandwich T-joint. Composite Structures , 460–468.
Kuo, J.-C., Chou, C.-W., Chang, C.-P., & Hung, H.-C. (2017). FORMOSAT-5 satellite Structure Development and Dynamic Launch Environment Verification. 68th International Astronautical Congress (IAC). Adelaide, Australia.
Li, D., Wang, R., Qian, R., Liu, Y., & Qing, G. (2016). Static response and free vibration analysis of the composite sandwich structures with multi-layer cores. International Journal of Mechanical Sciences , 101-115.
Maythraza, M., Anitha, D., Dash, P. K., & Kumar, P. R. (2018). Vibration analysis of honeycomb sandwich panel in spacecraft structure. International Journal of Mechanical and Production Engineering Research and Development, 8(3), 849-860.
Ontac, S., Dag, S., & Gokler, M. (2007). Structural Finite Element Analysis of stiffened and honey comb panels of RASAT satellite. 3rd International IEEE Conference on Recent Advances in Space Technologies.
Rice, R. C., Jackson, J. L., Bakuckas, J., & Thompson, S. (2003). Metallic Materials Properties Development and Standardization. Washington, D.C.: Office of Aviation Research.
Safarabadi, M., & Bazargan, S. (2015). Prediction of equivalent static loads act on a micro satellite via modal analysis. Engineering Solid Mechanics, 3(2), 75-84.
Sairajan, K., & Nair, P. (2010). Design of low mass dimensionally stable composite base structure for a spacecraft. Journal of Composites: Part B , 280-288.
Sun, W. Q., & Cheng, W. (2017). Finite element model updating of honeycomb sandwich plates using a response surface model and global optimization technique. Structural and Multidisciplinary Optimization, 55(1), 121-139.
Wagih, A., Hegaze, M. M., & Kamel, M. A. (2016). Pre-testing Analysis of large remote sensing satellite’s structure. AIAA SPACE 2016. Long Beach, California, USA.
Zheng, K., Liao, W. H., & Qin, Y. T. (2010). Analysis and Research of Honeycomb Sandwich structure for microsatellite based on equivalent theory. In Key Engineering Materials (Vol. 426, pp. 472-476). Trans Tech Publications.