RESISTOJET propulsion system for small satellite
2019 9th International Conference on Recent Advances in Space …, 2019•ieeexplore.ieee.org
Due to the launch safety constraints placed on Space companies built microsatellites,
designing a simple and reliable propulsion system with performance and characteristics in
line with the typical requirements of microsatellites presents a significant challenge to
aspiring engineers. This paper presents the design process of a low-cost, propulsion system
with a two-phase high density propellant. The aim of this study is the preliminary design of a
50mN RESISTOJET system operating at low pressure. The preliminary design and the …
designing a simple and reliable propulsion system with performance and characteristics in
line with the typical requirements of microsatellites presents a significant challenge to
aspiring engineers. This paper presents the design process of a low-cost, propulsion system
with a two-phase high density propellant. The aim of this study is the preliminary design of a
50mN RESISTOJET system operating at low pressure. The preliminary design and the …
Due to the launch safety constraints placed on Space companies built microsatellites, designing a simple and reliable propulsion system with performance and characteristics in line with the typical requirements of microsatellites presents a significant challenge to aspiring engineers. This paper presents the design process of a low-cost, propulsion system with a two-phase high density propellant. The aim of this study is the preliminary design of a 50mN RESISTOJET system operating at low pressure. The preliminary design and the optimization of the thruster dimensions are presented.
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