[1] R. W. Humble, N. H. Gary, and W. J. L. Lardon, Space Propulsion Analysis and Design, 1rd ed. New York: McGraw-Hill, 2007.
[2] M. Negri, "Replacement of hydrazine: Overview and first results of the H2020 project rheform," in 6th European Conference for Aeronautics and Space Sciences (EUCASS), Krakow, Poland, 2015.
[3] A. Okninski et al., "Development of green storable hybrid rocket propulsion technology using 98% hydrogen peroxide as oxidizer," Aerospace, vol. 8, no. 9, 2021, Art. no. 234, https://doi.org/10.3390/aerospace8090234.
[4] J. R. Wallbank, P. A. Sermon, A. M. Baker, L. Courtney, and R. M. Sambrook, "Nitrous oxide as a green monopropellant for small satellites," in 2th Conference on Green Propellants for Space Propulsion, Cagliari, Sardinia, Italy, 2004.
[5] Z. Vadim and L. Li, "Propulsion challenges for small spacecraft: 2005," Tsinghua Science and Technology, vol. 11, no. 5, pp. 507-514, 2006, https://doi.org/10.1016/S1007-0214(06)70227-9.
[6] R. Masse, J. Overly, M. Allen, and R. A. Spores, "A new state-of-the-art in Af-M315E thruster technologies," in 48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Atlanta, Georgia, 2012, Paper AIAA2012-4335, https://doi.org/10.2514/6.2012-4335.
[7] N. Wingborg, A. Larsson, M. Elfsberg, and P. Appelgren, "Characterization and ignition of ADN-based liquid monopropellants, in
41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Tucson, Arizona, 2005, Paper AIAA 2005-4468, https://doi.org/10.2514/6.2005-4468.
[8] A. E. S. Nosseir, A. Cervone, and A. Pasini, "Modular impulsive green monopropellant propulsion system (MIMPS-G): For CubeSats in LEO and to the Moon," Aerospace, vol. 8, no. 6, 2021, Art. no. 169, https://doi.org/10.3390/aerospace8060169.
[9] K. I. Parker and D. C. Folta, "15- Propulsion system," in Cubesat Handbook, From Mission Design to Operations, C. Cappelletti, S. Battistini, and B. K. Malphrus, Eds. Academic Press, 2020, pp. 283-301, https://doi.org/10.1016/B978-0-12-817884-3.00015-1.
[10] A. S. Gohardani et al., "Green space propulsion: Opportunities and prospects," Progress in Aerospace Sciences, vol. 71, pp. 128-149, 2014, https://doi.org/10.1016/j.paerosci.2014.08.001.
[11] S. Krishnan, A. S. Hee, and L. C. Won, "Design and development of a hydrogen-peroxide rocket-engine facility," Jurnal Mekanikal, no. 30, pp. 24-36, 2010.
[12] A. De laco Veris, Fundamental Concepts of Liquid-Propellant Rocket Engines," Springer Cham, 2021, https://doi.org/10.1007/978-3-030-54704-2.
[13] T. Franken, F. Valencia-Bel, B. V. S. Jyoti, and B. T. C. Zandbergen, "Design of a 1-N monopropellant thruster for testing of new hydrogen peroxide decomposition technologies," in Aerospace Europe Conference, Bordeaux, France, 2020, pp. 25-28.
[14] B. T. C. Zandbergen, "Thermal rocket propulsion," (version 2.04), Delft University of Technology, 2010, AE4S01, Lecture Notes.
[15] K. V. Mani, "Combined chemical-electric propulsion design and hybrid trajectories for stand-alone deep-space CubeSats," Ph.D. dissertation, Politecnico di Milano, Italy, 2020.
[16] A. K. Coker, Fortran Programs for Chemical Process Design, Analysis, and Simulation, Houston: Gulf, 1995.
[17] O. Bey and G. Eigenberger, "Fluid flow through catalyst filled tubes," Chemical Engineering Science, vol. 52, no. 8, pp. 1365-1376, 1997, https://doi.org/10.1016/S0009-2509(96)00509-X.
[18] G. P. Sutton and O. Biblarz, Rocket Propulsion Elements,9th ed. John Wiley & Sons, 2016.
[19] A. H. Adami, M. Mortazavi, and M. Nosratollahi, "Multidisciplinary design optimization of hydrogen peroxide monopropellant propulsion system using GA and SQP," International Journal of Computer Applications, vol. 113, no. 9, pp. 14-21, 2015, https://doi.org/10.5120/19853-1774.
[20] J. R. Wertz, D. F. Everett, and J. J. Puschell, Space Mission Engineering : the New SMAD, Hawthorne, CA: Microcosm Press, 2011.
