Large Spacecraft Electric Propulsion Using Multiphase Generator

A high-power high-voltage electric propulsion system for spacecrafts is proposed in this paper. For the spacecrafts with power levels below 10 kW, the conventional propulsion systems such as photovoltaic (PV) solar with battery energy storage, fuel cell, and radioisotope thermoelectric generator (RT...

Full description

Saved in:
Bibliographic Details
Published in2023 IEEE Aerospace Conference pp. 1 - 8
Main Authors Beik, Omid, Patel, Mukund R., Talebzadeh, Sarah
Format Conference Proceeding
LanguageEnglish
Published IEEE 04.03.2023
Subjects
Online AccessGet full text

Cover

Loading…