A.Kamran, G. Liang, R. Amer, N.Saima, Z. Qasim., Star grain optimization using genetic algorithm, In 51st AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference 18th AIAA/ASME/AHS Adaptive Structures Conference, 12th, p. 3084. 2010.
 M.Barrere, et al, Rocket Propulsion. Amsterdam, Elsevier Publishing Company, 1960.
 A. Ricciardi, Generalized geometric analysis of right circular cylindrical star perforated and tapered grains, Journal of Propulsion and Power, Vol.8, No.1, pp51-58, 1992.
 W. Guanglin,E. Cai, The design of Solid rocket motor, Published by Northwestern Polytechnical University Press, 1994.
 M. W. Stone, A Practicle Mathematical Approach to Grain Design. . ARS Semi- Annual meeting San Francisco, 1957.
 A. V. Jean, Recent Advances in Solid Propellant Grain Design., ARSJ, July 1959.
 W.T.Brooks, Ballistic Optimization of the Star Grain Configuration . Journal of Space craft, Vol. 19, No. 1, Jan–Feb, 1982.
 D. Wang, F. Yang, H. Fan,Z. Wei-Hua, An integrated framework for solid rocket motor grain design optimization, Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 228, no. 7, pp. 1156-1170, 2014.
 S. Mesgari, M. Bazazzadeh, A. Mostofizadeh, Finocyl grain design using the genetic algorithm in combination with adaptive basis function construction, International Journal of Aerospace Engineering, 3060173, 2019.
 S. Mesgari, M. Bazazzadeh, A. Mostofizadeh, Comparing Metamodel Methods of Adaptive Basis Function Construction and Artificial Neural Network in Finocyl Grain Design. Modares Mechanical Engineering. Dec 10;20(1), pp.45-56, 2019.
 A. Mahjub, N. M. Mazlan, M. Z. Abdullah, Q. Azam, Design Optimization of Solid Rocket Propulsion, A Survey of Recent Advancements." Journal of Spacecraft and Rockets, 57, no. 1 pp. 3-11, 2020.
 A. Almostafa, L. Guozhu, Two dimensional star grain optimization method using genetic algorithm, In 2018 15th International Bhurban Conference on Applied Sciences and Technology (IBCAST), pp. 158-165. IEEE, 2018.
 D. B. Riddle, R. J. Hartfield, J. E. Burkhalter, R.M. Jenkins, Genetic algorithm optimization ofliquid propellant missile systems, in: Proceedings of the AIAA Aerospace Sciences Meeting and Exhibit, AIAA, no.5506, 2009.
T.Ceyhun, M. Nikbay, Internal Ballistic Modeling of a Solid Rocket Motor by Analytical Burnback Analysis, Journal of Spacecraft and Rockets 56, no. 2,pp. 498-516, 2018.
 R. A. Saulius, F. E. Algimantas, S. U. Arvydas, Numerical Study on Internal Ballistics Characteristics of a Solid Propellant Rocket Motor, Mechanics. No. 1;25(3), pp. 187-96, 2019.
M. M. Ionut, Solid rocket motor internal ballistics simulation using different burning rate models, UPB Scientific Bulletin, no. 76 , pp.51-56, 2014.
T. Ceyhun, M. Nikbay, Solid Rocket Motor Propellant Optimization with Coupled Internal Ballistic–Structural Interaction Approach, Journal of Spacecraft and Rockets, vol.55, no. 4, pp. 936-947, 2018.
 O. Osemwengie, S. A. Abdallah, H. P. Morgan, J. O. Fanegan, Parameters Influencing Regression Rate of Solid Rocket Fuels. Int J Aeronautics Aerospace Res, no. 9;6(1), pp. 164-70, 2019
 L. Arnon, F. Bouquet, R. Sprik, Solid propellant grain geometry design, a model for the evolution of star shaped interfaces, Bachelor Thesis. Faculteit der Exacte Wetenshappen, Universiteit van Amsterdam (2010).
S. Patan. Design and geometrical analysis of propellant grain configurations of a solid rocket motor, 2014.
A.Lefebvre,Burning analysis of starconfiguration, 2000.
 M. R. Heidari, A. H. Adami, General Grain Analysis and Rapid Internal Ballistic Simulation for Solid Motor, Iranian Scientific Association of Energetic Material,.no. 5 (2), pp. 59-72, 2011, [in Persian]
 H. H. Hosseni, Geometric Analysis of Grian Types. Aerospace Organization. Shahid Yazdani Institute. Propulsion Technology Research Center, 1384[in Persian]
 O. Yucel., Ballistic design optimization of three-dimensional grains using genetic algorithms, Master's thesis, 2012.