[1] Turner, J.L Martin., Rocket and spacecraft propulsion, Department of physics and Astronomy, University of Leicester, Leicester, UK, Praxis Publishing,2006.
[2] Sutton G. P., Oscar B., "Rocket Propulsion Elements", 7th edition, Wiley Inter. science, New York, 2001.
]3[کریمی.ح، آیروترمودینامیک موتور موشک، دانشکده هوافضا، دانشگاه صنعتی خواجه نصیرالدین طوسی،1379 (جزوه درسی)
[4] Gordon C. O., Aerothermodynamics Of Gas Turbine And Rocket Propulsion, Third Edition, AIAA Education Series, 1998.
[5] Bertrand, Capt., Brinley, R., Rocket Manual for Amateurs, Ballantine Books, 1964.
[6] M. Johannsson, Optimization of Solid Rocket Grain Geometries, Master of Science Thesis Report in Aerospace Engineering, Royal Institute of Technology (KTH), Stockholm, Sweden, 2012.
[7] Davenas A, Solid Rocket Propulsion Technology, Technology and Research Director, SNPE, France, 1993.
[8] Brown, B., A Guide to Amateur Rocketry, U.S.Army, Fort Sill Oklahoma, 1965.
[9] Chin, S.S, Missile Configuration Design, McGraw-Hill, 1961
[10] Nielsen, N. Jack, Missile Aerodynamics, McGraw-Hill, California, 1960.
[11] Singh, S. Solid Rocket Motor for Experimental Sounding Rockets, Advances in Aerospace Science and Applications, Research India Publication, Vol. 3, No. 3, 2013.
[12] Meyerowitz, G. Experimental Rocket Motor Safety & Standards Manual, YPL Director in Yale University, June 2013.
[13] Terzic J.,. Zecevic B, Baskarad M., Catovic A., sabina S. K., Prediction of internal ballistic parameters of solid propellant rocket motors, 8th international armament Conference, Poland,2010.
]14[فولادی نوربخش، زین العابدینی احمد، فرآیند طراحی مفهومی سامانههای پیشرانش سوخت جامد، پروژه افق گزارش(1-17)، دانشگاه صنعتی مالک اشتر، مرکز تحقیقات فضایی، 1386.
]15[فولادی نوربخش، اصول طراحی سامانههای پیشران سوخت جامد ، انتشارات دانشگاه صنعتی مالک اشتر، تهران، 1389.
[16] Morgan G. C., An Investigation into the combustion and performance of small solid propellant rocket motors, Aeronautical Engineering Project, Thesis and Practical Experience, University of New South Wales- Australian Defense Force Academy,2008.
[17] MSFC-DOC-1622, Advanced Solid Rocket Motor Design and Performance Requirement Document, G.C. Marshal Space Flight Center, Alabama.
[18] NASA, Solid Propellant Selection and Characterization, NASA SP-8064, June 1971.
[19] NASA, Solid Propellant Grain Design and Internal Ballistic, NASA SP-8076, March1972.
[20] Fry, R.S, Solid Propellant Test Motor Scaling, CPIA, 2001.
[21] Nakka, A. Richard, Solid Propellant Rocket Motor Design and Testing, Thesis, the University of Manitoba, 1984.
[22] Fleeman, L. Eugene, Tactical Missile Design, AIAA, 2001.
[23] RAS Aero manual, 2011.
[24] Brown, B., A Guide To Amateur Rocketry, U.S.Army, Fort Sill Oklahoma, 1965.
[25] RYCHKOV, A.D., Design Of Optimal Contours Of Supersonic Parts Of Solid Propellant Motor Nozzles With Use Of Direct Variational Methods”, Institute of Computational Technologies SB RAS, Thermophysics and Aeromechanics, Vol. 13, No. 1, Novosibirsk, Russia, 2006.
[26] Knauber, R. N., Thrust Misalignments of Fixed-Nozzle Solid Rocket Motors, Lockheed Martin Vought System, Journal Of Spacecraft And Rockets, , Dallas, Texas, November-December 1996.
[27] Merrill K. King, Erosive Burning Of Composite Propellants, Atlantic research Corporation, U.S, Virginia, 1976.
[28] Merrill K. King, Erosive Burning of Composite Propellants: Experimental and modeling Studies, Atlantic research Corporation, Alexandria, Virginia, 1978.
[29] Jacib. Dennis, James. Villarreal, A primer for University level solid rocket motor research and development, AIAA Aerospace Sciences, 2010 Florida.
[30] Bertrand, Capt., Brinley, R., Rocket Manual for Amateurs”, Ballantine Books, 1964.
[31] Dennis J., Villarreal J. K., Design and Validation Testing of the Sol-Brid Rocket Motor, 49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, Florida, 2011.
[32] Cannon, B., Igniters and their use, Estes- Cox Corporation, EstesEducator.com, 2012.
[33] Morrow, R. B., Pines, M. S., Small Sounding Rockets, Small Rockets Press, 2000.
[34] NASA, Captive-Fired Testing of Solid Rocket Motors, NASA SP-8041, NASA Space Vehicle Design Criteria, March 1971.
)