[1] Mirshams, M., Karimi, H. and Naseh, H., “Algorithm to Determine the Optimal Mass Distribution Liquid Propellant Launch Vehicle”, Sixth National Conference of Iranian Aerospace Society, K. N. Toosi University of Technology, 2007 (In Persian).
[2] Space Launch System and Ground to groundballistic Missiles Report, PBRM Software, Aerospace Industry Organization, 2006.
[3] Mirshams, M. and Naseh, H., “Guidelines for school projects Launch Vehicle Design”, Publications Department of Aerospace Engineering, K. N. Toosi University of Technology ,winter. 2007 (in Persian).
[4] Mirshams, M., Karimi, H. and Naseh, H., “Multi-Stage Liquid Propellant Launch Vehicle ConceptualDesign (LVCD) Software Based on Combinatorial Optimization of Major Design Parameters”, Journal ofSpace Science and Technology (JSST), Winter 2009, pp.17-25 (in Persian).
[5] Mirshams, M., Mirdamadian, M., Naseh, H. and Fazeli, H. R., “Closed Cycle Liquid Propellant Parameters Design Optimization using Response Surface Methods”, The first Conference of Launch Vehicle Systems, K.N.Toosi University of Technology, 2011 (in Persian).
[6]M. Akhlaghi, H. Naseh, M. Mirshams, S. Irani, “A Bayesian Networks Approach to Reliability Analysis of a Launch Vehicle Liquid Propellant Engine,” Journal of Aerospace and Technology, Vol. 3-30, No. 1, (JAST), 2012.
[7] M. Mirshams, H. Naseh, M. Mirdamadian, H. R. Fazeli, “The Sensitivity Analysis Engine System Parameters In Liquid Propellant Launch Vehicle”, K.N.Toosi University of technology, The first Conference of Satellite Systems, 2011 (in Persian).
[8] M. Mirshams, H. Naseh, H. R. Fazeli, “Multi-objective Multidisciplinary Design of Space Launch System using Holistic Concurrent Design”, Journal of Aerospace, Science and Technology, Vol. 33, Issue 1, Feb. 2014, pp. 40–54.
[9] Feodosev, V., Translated by: Roshanian, J., Mirshams, Karimi, M. H., Introduction to Misslie Design, K. N. Toosi University of Technology Inc., 2000.
[10] Mirshams, M., Naseh, H. and Fazeli, H.R., “Multi-objective Multidisciplinary design of Space Launch System using Holistic Concurrent Design”, Journal of Aerospace, Science and Technology, Vol. 33, Issue 1, 2014, pp. 40–54
[11] Jodei,J., EbrahimiM., and RoshanianJ., “Multidisciplinary Design Optimization of a Small Solid Propellant Launch Vehicle Using System Sensitivity Analysis”, Journal of Structural and Multidisciplinary Optimization, Vol. 38, 2009, pp. 93–100.
[12] Dehkordi, S.Y. Mirshams, M. and Roshanian, J. “Launch Vehicle Collaborative Robust Optimal Design with Multiobjective Aspect and Uncertainties”, Journal of Modares Mechanical Engineering,Vol. 15, No. 11, pp. 339-350 (in Persian).
