Optimization of Geostationary Orbit Transfers via Combined Chemical–Electric Propulsion
For geostationary orbit transfers, a long duration is required using electric propulsion and a large propellant mass is needed with chemical propulsion. Hybrid transfers can achieve a balance between the fuel consumption and transfer time. In this paper, a trajectory optimization method is proposed...
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| Autori principali: | , , |
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| Natura: | Artigo |
| Lingua: | Inglês |
| Pubblicazione: |
MDPI AG
2022-04-01
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| Serie: | Aerospace |
| Soggetti: | |
| Accesso online: | https://www.mdpi.com/2226-4310/9/4/200 |
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