A Coaxial Pulsed Plasma Thruster Model with Efficient Flyback Converter Approaches for Small Satellites

Pulsed plasma thrusters (PPT) have demonstrated enormous potential since the 1960s. One major shortcoming is their low thrust efficiency, typically <30%. Most of these losses are due to joule heating, while some can be attributed to poor efficiency of the power processing units (PPUs). We model PPTs...

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Principais autores:	Dillon O’Reilly, Georg Herdrich, Felix Schäfer, Christoph Montag, Simon P. Worden, Peter Meaney, Darren F. Kavanagh
Formato:	Artigo
Idioma:	Inglês
Publicado em:	MDPI AG 2023-06-01
coleção:	Aerospace
Assuntos:	flyback thruster pulsed plasma space electric
Acesso em linha:	https://www.mdpi.com/2226-4310/10/6/540
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