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• W4386548984 abstract "This chapter is about the electric propulsion (EP) for CubeSats, both state-of-the-art and future perspectives are discussed. An EP system can be defined as a thruster in which a gas is accelerated by means of electrical heating and/or electric and magnetic body forces. Provided that the thrust is generated employing electric power, which is limited on board of satellites, EP systems have two common characteristics: the thrust is low (<1 N) and the specific impulse is high (up to 10,000 s). Thus, the use of electric thrusters has a major impact on a space mission: maneuvers can be accomplished with relatively little propellant and systems can be operated, rather in a continuous or pulsed regime, for long durations (up to years). For these reasons, EP systems enable totally new mission scenarios not possible with chemical thrusters. EP subsystems include the Power Processing Unit (PPU), propellant management, and thermal control. In this chapter, only high-level aspects of EP are analyzed. Discussions about tanks, pressure regulators, valves, and sensors have not been included." @default.
• W4386548984 created "2023-09-09" @default.
• W4386548984 creator A5004355574 @default.
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• W4386548984 date "2023-01-01" @default.
• W4386548984 modified "2023-10-16" @default.
• W4386548984 title "Electric propulsion systems" @default.
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• W4386548984 doi "https://doi.org/10.1016/b978-0-12-824541-5.00018-2" @default.
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