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Interplanetary Mission Performance Assessment of a TANDEM Electric Thruster-Based Spacecraft

The aim of this paper is to analyze the transfer performance of a spacecraft equipped with a TANDEM electric propulsion system in a classical interplanetary mission scenario targeting Mars, Venus, or a near-Earth asteroid. The TANDEM concept is a coaxial, two-channel Hall-effect thruster recently pr...

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Autor Principal: Alessandro A. Quarta
Formato: Artigo
Idioma:Inglês
Publicado: MDPI AG 2025-11-01
Series:Applied Sciences
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Acceso en liña:https://www.mdpi.com/2076-3417/15/21/11711
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