On helicon thrusters: Will they ever fly?
Valery Godyak
Abstract
Valery Godyak
Abstract
The feasibility of helicon plasma thrusters, commonly considered the most promising for deep space propulsion, is evaluated in terms of their plasma production efficiency, longevity, operation stability, and need for massive magnets with large power consumption. It is shown that helicon thrusters should be inferior to those based on inductively coupled plasmas.
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The feasibility of helicon plasma thrusters, commonly considered the most promising for deep space propulsion, is evaluated in terms of their plasma production efficiency, longevity, operation stability, and need for massive magnets with large power consumption. It is shown that helicon thrusters should be inferior to those based on inductively coupled plasmas.
Key concepts: Helicon, Propulsion, Plasma, Spacecraft propulsion, Electrically powered spacecraft propulsion, Ion thruster, Power consumption, Magnet