Thrust Model and Trajectory Design of an Interplanetary CubeSat with a Hybrid Propulsion System
This paper analyzes the performance of an interplanetary CubeSat equipped with a hybrid propulsion system (HPS), which combines two different types of thrusters in the same deep space vehicle, in a heliocentric transfer between two assigned (Keplerian) orbits. More precisely, the propulsion system o...
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| Format: | Artigo |
| Sprache: | Inglês |
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MDPI AG
2024-10-01
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| Schriftenreihe: | Actuators |
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| Online-Zugang: | https://www.mdpi.com/2076-0825/13/10/384 |
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