Design and control of high voltage gain DC–DC converter for CubeSat propulsion

Author:

Ouhammam AbdelaaliORCID,Mahmoudi Hassane,Ouadi Hamid

Publisher

Springer Science and Business Media LLC

Subject

Space and Planetary Science,Aerospace Engineering

Reference16 articles.

1. Woellert, K., Ehrenfreund, P., Ricco, A., Hertzfeld, H.: Cubesats: cost-effective science and technology platforms for emerging and developing nations. Adv. Space Res. 47, 663–684 (2011). https://doi.org/10.1016/j.asr.2010.10.009

2. Tummala, A.R., Dutta, A.: An overview of cube-satellite propulsion technologies and trends. Aerospace 4, 58 (2017). https://doi.org/10.3390/aerospace4040058

3. Ralph, A., Hsu, A., Young, J., Curtiss, T.: Characterization of a Single Emitter Electrospray Thruster (2016). 10.13140/RG.2.2.28585.24165

4. Tacon, C.: Applications and Principles of Electrospray Spacecraft Propulsion (2019)

5. Ma, C., and Ryan, C. N.: The Design and Characterization of a Porous-emitter Electrospray Thruster (PET-100) for Interplanetary CubeSats. In 7th Interplanetary CubeSat Workshop, pp. 01309-01309 (2018)

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1. High-performance, miniaturized and configurable power and control unit for electrospray thrusters;CEAS Space Journal;2024-07-25

2. Realization and control of a high voltage gain DC-DC converter for CubeSat electric propulsion;2024 International Conference on Global Aeronautical Engineering and Satellite Technology (GAST);2024-04-24

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