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Information × Registration Number 0226U002913, (0124U001264) , R & D reports Title Vacuum-arc thruster of CubeSat satellites for the organization of an efficient system of data collection and exchange popup.stage_title Розробка конструкції вакуумно-дугового двигуна Head Breus Andrii O, к.т.н. Registration Date 09-03-2026 Organization National Aerospace University "Kharkiv Aviation Institute" popup.description1 Design and manufacture a prototype of a vacuum-arc thruster for CubeSat-type satellites with an engine thrust in impulse of at least 10 μN, a specific impulse of at least 1000 s, and a volume (together with the electrical power system) of no more than 0.3 U popup.description2 Within the reporting stage of the research and development project, a set of results was obtained aimed at advancing plasma technologies, nanomaterials science, and electric propulsion systems for space applications. The interaction of a low – energy electron beam with beam-sensitive materials was studied using crystalline gold trichloride as a model system. The experiments revealed mechanisms of carbon nanostructure formation on the surface and phase transformations in the near-surface volume, which significantly affect the accuracy of electron microscopy and compositional analysis. A new plasma-initiated approach for the controlled transformation of nanomaterials from one – dimensional to two – dimensional structures was proposed, providing new opportunities for tailoring material properties. The prospects of plasma – based technologies for additive manufacturing under space conditions were analyzed, highlighting their potential for autonomous fabrication and repair in vacuum and microgravity environments. A non – contact system for measuring the surface temperature during vacuum-arc coating deposition was developed, enabling real – time control of thermal conditions. An impulse vacuum-arc plasma source for multicomponent coatings was created. In addition, a power supply unit for a vacuum – arc thruster, a signal conditioning module, and a prototype thruster were developed. Vacuum chamber tests confirmed the operational stability and feasibility of the proposed technical solutions. Product Description popup.authors Serhii L. Abashyn Oleh O. Baranov Oleksandr M. Hnytko Oksana V. Kosenko Nataliia I. Kot Ihor I. Kuchynskyi Volodymyr I. Nazin Vasyl I. Ruzaikin Yurii O. Sysoiev Olena V. Torosian Olha V. Shypul Yurii V. Shyrokyi Yelizaveta O. Baranova popup.nrat_date 2026-03-09 Close