[1] W. Ley, K. Wittmann, and W. Hallmann, Handbook of space technology. John Wiley & Sons, 2009.
[2] C. D. Brown, Spacecraft propulsion. Aiaa, 1996.
[3] D. Altman and D. D. Thomas, "Evaluation of Hydrazine as a Monopropellant and a Gas Generant," 1949.
[4] A. Grant, "Development of Hydrazine as Monopropellant and Gas Generant," Jet Propulsion Laboratory, California Institute of Technology Rept, pp. 9-1, 1950.
[5] E. Wucherer, T. Cook, M. Stiefel, R. Humphries, and J. Parker, "Hydrazine catalyst production-sustaining S-405 technology," in 39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, 2003, p. 5079. Available: https://doi.org/10.2514/6.2003-5079
[6] K.-H. Lee, M.-J. Yu, S.-K. Kim, K.-W. Jang, and S.-J. Cho, "Hot Firing Performance Measurement of Monopropellant Decomposition Catalyst and Domestic Development Status," Journal of the Korean Society of Propulsion Engineers, vol. 10, no. 3, pp. 109-117, 2006.
[7] P. McRight, C. Popp, C. Pierce, A. Turpin, W. Urbanchock, and M. Wilson, "Confidence testing of Shell-405 and S-405 catalysts in a monopropellant hydrazine thruster," in 41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 2005, p. 3952. Available: https://doi.org/10.2514/6.2005-3952
[8] A. Kersten, "Analytical Study of Catalystic Reactors for Hydrazine Decomposition, Part 1. Steady State Behavior," NASA Contract NAS, pp. 7-458, 1966.
[9] V. Shankar, K. A. Ram, and K. Bhaskaran, "Prediction of the concentration of hydrazine decomposition products along a granular catalytic bed," Acta astronautica, vol. 11, no. 6, pp. 287-299, 1984. Available:https://doi.org /10.1016/0094-5765(84)90038-9
[10] H. Hearn and D. Young, "Performance prediction model for a high-impulse monopropellant propulsion system," Journal of Spacecraft and Rockets, vol. 11, no. 11, pp. 764-768, 1974. Available: https://doi.org/ 10.2514/3.27790
[11] H. Hearn, "Flight performance of a high-impulse monopropellant thruster," Journal of Spacecraft and Rockets, vol. 13, no. 5, pp. 261-265, 1976. Available: https://doi.org/10.2514/3.27905
[12] S. Garg, "Empirical simulation model for hydrazine attitude control thrusters," Journal of Spacecraft and Rockets, vol. 16, no. 6, pp. 389-393, 1979.
[13] V. Shankar, K. A. Ram, and K. Bhaskaran, "Experimental investigations of the 10 N catalytic hydrazine thruster," Acta Astronautica, vol. 12, no. 4, pp. 237-249, 1985. Available:https://doi.org/10.1016/0094-5765(85)90038-4
[14] J. Hinckel, J. Jorge, T. Soares, M. Zacharias, and J. Palandi, "Low cost catalysts for hydrazine monopropellant thrusters," in 45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 2009, p. 5232. Available: https://doi.org/10.2514/6.2009-5232
[15] H. Karimaei, M. R. Salimi, H. Naseh, and E. Jokari, "Design of Physical Configuration of a 10N Monopropellant Hydrazine Thruster," Journal of Space Science and Technology, vol. 12, pp. 13-22, 2019 (in Persian).
[16] H. Karimaei, R. Ghorbani, and S. M. Hosseinalipour, "Implementation of linear stability theory on hollow cone-shaped liquid sheet," Periodica Polytechnica Mechanical Engineering, vol. 64, no. 3, pp. 179-188, 2020. Available: https://doi.org/10.3311/PPME.11727
[17] F. Ommi, Design Principles of space engines and propulsion, Tarbiat Modares University, tehran, 2017 (in Persian).
[18] S. Hosseinalipour, H. Karimaei, and R. Ghorbani, "study the Y-atomizer performance of a power plant in order to extract mean droplet diameter range," 2nd proceedings of gas turbine, 2013.
[19 H. Karimaei, "Design and Simulation of Fuel Injector of a 10N Monopropellant Hydrazine Thruster," Journal of Space Science and Technology, vol. 11, pp. 9-19, 2018 (in Persian).
[20] M. Salimi, "Numerical Study of Catalyst Bed Length and Particle Size Effect on the Monopropellant Thruster Specific Impulse and Thrust," Scientific Journal of, 2020 (in Persian).
[21] M. R. Salimi, "Effects of geometrical parameters of a two-sided catalyst bed on flow and thermal fields of a monopropellant hydrazine thruster," Space Science and Technology, vol. 15, pp. 93-110, 2022 (in Persian)