How to cite this paper
Sabaghzadeh, H & Khansari, N. (2022). Optimal design of four stage launch vehicle considering multi objective NSGA II algorithm and mass-energetic concepts.Engineering Solid Mechanics, 10(3), 269-286.
Refrences
Balesdent, M., Bérend, N., Dépincé, P., & Chriette, A. (2012). A survey of multidisciplinary design optimization methods in launch vehicle design. Structural and Multidisciplinary Optimization, 45(5), 619-642. doi: 10.1007/s00158-011-0701-4
Bennett, D. (2019). Design of a Nozzle for the Spyder 2nd Stage Solid Rocket Motor.
Bhatnagar, P., Rajan, S., & Saxena, D. (2012). Study on optimization problem of propellant mass distribution under restrictive condition in multistage rocket. Paper presented at the International Conference on Advances in Computer Applications (ICACA).
Braun, R., Moore, A., & Kroo, I. (1996). Use of the collaborative optimization architecture for launch vehicle design. Paper presented at the 6th Symposium on Multidisciplinary Analysis and Optimization.
Bruhn, E. F. (1967). Analysis and design of missile structures.
Cormier, T., Scott, A., Ledsinger, L., McCormick, D., Way, D., & Olds, J. (2000). Comparison of collaborative optimization to conventional design techniques for a conceptual RLV. Paper presented at the 8th Symposium on Multidisciplinary Analysis and Optimization.
Da Cás, P. L. K., Vilanova, C. Q., Barcelos Jr, M. N. D., Veras, C. A. G. J. J. o. A. T., & Management. (2012). An optimized hybrid rocket motor for the SARA platform reentry system. 4(3), 317-330.
Deb, K., Pratap, A., Agarwal, S., & Meyarivan, T. J. I. t. o. e. c. (2002). A fast and elitist multiobjective genetic algorithm: NSGA-II. 6(2), 182-197.
Fakoor, M., & MEHRE, N. (2016). Simulation of orthotropic damaged zone behavior using viscoelastic models. Amirkabir Journal of Mechanical Engineering, 48(4), 401-410.
Fakoor, M., Sabour, M., & Khansari, N. (2014). A new approach for investigation of damage zone properties in orthotropic materials. Engineering Solid Mechanics, 2(4), 283-292.
Hammond, W. E. (2001). Design methodologies for space transportation systems: Aiaa.
He, L. (2002). Ballistic missiles and launch vehicles design: 北京航空航天大学出版社.
Khansari, N., Farrokhi, A., & Mosavi, A. (2019). Orthotropic mode II shear test fixture: Iosipesque modification. Engineering Solid Mechanics, 7(2), 93-108.
Mirshams, K., Naseh. ( 2008). Multi-Stage Liquid Propellant Launch Vehicle Conceptual Design, Based on Combinatorial Optimization of Major Design Parameters. J. J. o. S. Science and Technology, 1(1).
Norris, R. S., & Kristensen, H. M. J. B. o. t. A. S. (2009). Nuclear US and Soviet/Russian intercontinental ballistic missiles, 1959-2008. 65(1), 62-69.
Roshanian, J., & Keshavarz, Z. J. C. J. o. A. (2007). Effect of variable selection on multidisciplinary design optimization: a flight vehicle example. 20(1), 86-96.
Shamsirband, S., & Mehri Khansari, N. (2021). Micro-mechanical damage diagnosis methodologies based on machine learning and deep learning models. Journal of Zhejiang University-SCIENCE A, 22(8), 585-608.
Tartabini, P. V., Wurster, K. E., Korte, J., Lepsch, R. A. J. J. o. S., & Rockets. (2002). Multidisciplinary analysis of a lifting body launch vehicle. 39(5), 788-795.
Tsuchiya, T., & Mori, T. (2002). Multidisciplinary design optimization to future space transportation vehicles. Paper presented at the AIAA/AAAF 11th International Space Planes and Hypersonic Systems and Technologies Conference, Orleans, France.
Tsuchiya, T., Mori, T. J. J. o. S., & Rockets. (2004). Optimal conceptual design of two-stage reusable rocket vehicles including trajectory optimization. 41(5), 770-778.
Villanueva, F. M., & Abbas, H. (2015). Small launch vehicle optimal design configuration from ballistic missile components. Paper presented at the 2015 12th International Bhurban Conference on Applied Sciences and Technology (IBCAST).
Woolf, A. F. (2009). US Strategic Nuclear Forces: Background, Developments, and Issues: Diane Publishing.
Bennett, D. (2019). Design of a Nozzle for the Spyder 2nd Stage Solid Rocket Motor.
Bhatnagar, P., Rajan, S., & Saxena, D. (2012). Study on optimization problem of propellant mass distribution under restrictive condition in multistage rocket. Paper presented at the International Conference on Advances in Computer Applications (ICACA).
Braun, R., Moore, A., & Kroo, I. (1996). Use of the collaborative optimization architecture for launch vehicle design. Paper presented at the 6th Symposium on Multidisciplinary Analysis and Optimization.
Bruhn, E. F. (1967). Analysis and design of missile structures.
Cormier, T., Scott, A., Ledsinger, L., McCormick, D., Way, D., & Olds, J. (2000). Comparison of collaborative optimization to conventional design techniques for a conceptual RLV. Paper presented at the 8th Symposium on Multidisciplinary Analysis and Optimization.
Da Cás, P. L. K., Vilanova, C. Q., Barcelos Jr, M. N. D., Veras, C. A. G. J. J. o. A. T., & Management. (2012). An optimized hybrid rocket motor for the SARA platform reentry system. 4(3), 317-330.
Deb, K., Pratap, A., Agarwal, S., & Meyarivan, T. J. I. t. o. e. c. (2002). A fast and elitist multiobjective genetic algorithm: NSGA-II. 6(2), 182-197.
Fakoor, M., & MEHRE, N. (2016). Simulation of orthotropic damaged zone behavior using viscoelastic models. Amirkabir Journal of Mechanical Engineering, 48(4), 401-410.
Fakoor, M., Sabour, M., & Khansari, N. (2014). A new approach for investigation of damage zone properties in orthotropic materials. Engineering Solid Mechanics, 2(4), 283-292.
Hammond, W. E. (2001). Design methodologies for space transportation systems: Aiaa.
He, L. (2002). Ballistic missiles and launch vehicles design: 北京航空航天大学出版社.
Khansari, N., Farrokhi, A., & Mosavi, A. (2019). Orthotropic mode II shear test fixture: Iosipesque modification. Engineering Solid Mechanics, 7(2), 93-108.
Mirshams, K., Naseh. ( 2008). Multi-Stage Liquid Propellant Launch Vehicle Conceptual Design, Based on Combinatorial Optimization of Major Design Parameters. J. J. o. S. Science and Technology, 1(1).
Norris, R. S., & Kristensen, H. M. J. B. o. t. A. S. (2009). Nuclear US and Soviet/Russian intercontinental ballistic missiles, 1959-2008. 65(1), 62-69.
Roshanian, J., & Keshavarz, Z. J. C. J. o. A. (2007). Effect of variable selection on multidisciplinary design optimization: a flight vehicle example. 20(1), 86-96.
Shamsirband, S., & Mehri Khansari, N. (2021). Micro-mechanical damage diagnosis methodologies based on machine learning and deep learning models. Journal of Zhejiang University-SCIENCE A, 22(8), 585-608.
Tartabini, P. V., Wurster, K. E., Korte, J., Lepsch, R. A. J. J. o. S., & Rockets. (2002). Multidisciplinary analysis of a lifting body launch vehicle. 39(5), 788-795.
Tsuchiya, T., & Mori, T. (2002). Multidisciplinary design optimization to future space transportation vehicles. Paper presented at the AIAA/AAAF 11th International Space Planes and Hypersonic Systems and Technologies Conference, Orleans, France.
Tsuchiya, T., Mori, T. J. J. o. S., & Rockets. (2004). Optimal conceptual design of two-stage reusable rocket vehicles including trajectory optimization. 41(5), 770-778.
Villanueva, F. M., & Abbas, H. (2015). Small launch vehicle optimal design configuration from ballistic missile components. Paper presented at the 2015 12th International Bhurban Conference on Applied Sciences and Technology (IBCAST).
Woolf, A. F. (2009). US Strategic Nuclear Forces: Background, Developments, and Issues: Diane Publishing.