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).
 Space Launch System and Ground to groundballistic Missiles Report, PBRM Software, Aerospace Industry Organization, 2006.
 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).
 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).
 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).
 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.
 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).
 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.
 Feodosev, V., Translated by: Roshanian, J., Mirshams, Karimi, M. H., Introduction to Misslie Design, K. N. Toosi University of Technology Inc., 2000.
 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
 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.
 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).