[1] Zakeri, M., Upper Stage (Transfer Block) Design, (M.Sc. Thesis), KNTU University, 1389 (In Persian).
[2] Hohmann, W., Die Erreichbarkeit der Himmelskiirper, R.Oldenbourg, Munich, 88 pp, 1925.
[3] Hoelker, R. F. and Silber, R., “The Bi-Elliptical Transfer Between Circular Coplanar Orbits,” Planetary and Space Science, Vol. 7, No. 1, 1959, pp. 164-175.
[4] Tsien, H. S., “Take-off from Satellite Orbit,” Journal of the American Rocket Society, Vol. 23, No. 4, 1953, pp. 233-236.
[5] Lawden, D. F., “Optimal Programming of Rocket Thrust Direction,” Acta Astronautica, Vol. 1, No. 1, 1955, pp.41-56.
[6] Biggs, M. C. B., “The Optimization of Spacecraft Orbital Manoeuvres, Part II: Using Pontryagin’s Maximum Principle,” The Hattfield Polytechnic, Numerical Optimization Centre, Hertfordshire, UK, 1979.
[7] Ceballos, D. C. and Rios-Neto, A., “Linear Programming and Suboptimal Solutions of Dynamical Systems Control Problems,” Procceding of the International Symposium on Spacecraft Flight Dynamics, Darmstadt, Federal Republic of Germany, 1981, pp. 239-244.
[8] Rios-Neto, A. and Bambace, L. A. W., “Optimal Linear Estimation and Suboptimal Numerical Solutions of Dynamical Systems Control Problems,” Proceding of the International Symposium on Spacecraft Flight Dynamics, Darmstadt, Fedral Republic of Germany, 1981, pp. 233-238.
[9] Lara, M. R., “ATK Space Propulsion Products Catalog,” Approved for Public Release OSR No. 08-S-0259 and OSR No. 08-S-1556, Dated 2008.
[10] Curtis, H., Orbital Mechanics for Engineering Students, Elsevier Ltd. Burlington, 2007.
[11] Kirk, D., Optimal Control Theory: An Introduction, Prentice-Hall, Englewood Cliffs, NJ, 1970.
[12] Ocampo, C., “Finite Burn Maneuver Modeling for a Generalized Spacecraft Trajectory Designand Optimization System,” Annals of the New York Academy of Sciences, Vol. 1017, Issue 1, 2004, pp. 210-233.
[13] Ocampo, C., “An Architecture for a Generalized Trajectory Design and Optimization System,” Proceedings of the International Conference on Libration Points and Missions, June 2002. Girona, Spain.
[14] McGill, R. and Kenneth, P. “A Convergence Theorem on the Iterative Solution of Nonlinear Two-Point Boundry-Value System,” Reprint of Paper Presented at the XIV International Astronatical Congress, Paris,France, 1963.
[15] McGill, R. and Kenneth, P. “Solution of Variational Problems by Means of a Generalized Newton-Raphson Operator,” AIAA Journal, Vol. 2, No. 10, 1964, pp. 1761-1766.
[16] Sutton, G. P. and Biblarz, O., Rocket Propulsion Elements, 7th Edition, John Wiley & Sons, 2001.
