[1] Yang, A.S., “Satellite Hydrazine Propulsion System Design Trades,” Journal of Da-Yeh University, Vol. 10, No. 1, 2001, pp. 41-50.
[2] Karimaei, H., “Design and Simulation of Fuel Injector of a 10N Monopropellant Hydrazine Thruster”, Journal of Space Science and Technology, Vol. 10, 2018, pp. 59-65 (in Persian).
[3] Meibody, M.N.P., Naseh and Ommi, H.F., Hydrazine, Monopropellant Catalyst Bed Optimization Methodology, the 16th International Conference of Iranian Aerospace Society, Tehran, 21-23,Feb 2017.
[4] Birbara, P.J. and Conn, W.L., Catalyst for Hydrazine Decomposition and the Method of Producing the Catalyst, US Patent 4324819, 1980.
[5] Soares Netoa, T.G., Cobob, A.J.G. and Cruz, G.M. “Evolution of Morphologic Properties on the Preparation of Ir/Al2O3 Catalysts with High Metallic Contents,” Applied Surface Science, Vol. 240, 2005, pp. 355–365.
[6] Armstrong, W.E., Ryland, L.B. and Voge, H.H., Catalyst for hydrazine decomposition and method for preparing such catalyst, US Patent 4124538, 1978.
[7] Kesten, A.S., Analytical Study of Catalytic Reactors for Hydrazine Decomposition, Quarterly Progress Report, No. 6, United Aircraft Research Laboratories, Contract NAS 7-458, 1968.
[8] Makled, A.E., Belal, H., “Modeling of Hydrazine Decomposition for Monopropellant Thrusters,” 13th International Conference on Aerospace Sciences & Aviation Technology, ASAT-13, May 26 – 28, 2009.
[9] Kesten, A.S., Analytical Study of Catalytic Reactors for Hydrazine Decomposition, Quarterly Progress Report No 2 Report E910461-6 United Aircraft Research laboratories, 1966.
[10] Shankar, V., and Anantha Ram, K., “Experimental Investigations of the 10 N Eatalytic Hydrazine Thruster,” Acta Astronautica, Vol. 12, No. 4, 1985, pp. 237-249.
[11] Estes, R H, “Development and Implementation of a Process for Producing a Highly Wettable Aluminum PMD for the GPM Hydrazine Tank,” 48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit (Atlanta, Georgia, 30 July-01 Aug 2012).
[12] Meibody, M.N.P., Naseh, H. and Ommi, F., “Hydrazine Monopropellant Catalyst Bed Optimization Methodology”, International Confrence of Iranian Aerospace Society, 2017.