More efficient RF plasma electric thruster
AssigneeNew England Space Works, Inc.
InventorLynn B. Olson
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AssigneeNew England Space Works, Inc.
InventorLynn B. Olson
Estimating the term…
A radio frequency (RF) plasma thruster for use in electric propulsion for spacecraft. The thruster operates by heating plasma in a magnetic field, which then flows out along magnetic field lines, producing axial thrust. The present invention greatly increases the efficiency of the RF plasma thruster compared to previous thrusters of this type, while retaining the advantages of RF plasma thrusters over other types of electric and chemical propulsion systems. The present invention utilizes a lower hybrid wave for heating of the electrons, rather than electron cyclotron resonance (ECR) heating. The lower hybrid wave is used because it creates high-density plasmas and the antennas used to couple RF energy to the plasma are relatively simple to construct. This allows much better efficiency because no hot electron population is created to siphon off much of the RF power applied to the plasma. Lower hybrid waves propagate in the frequency range between the ion cyclotron frequency and the electron cyclotron frequency. The RF thruster of the present invention has a higher specific impulse than electrothermal thrusters, much higher power density than electrostatic ion thrusters, no life limiting grids or electrodes in contact with the plasma, and a simple geometry which is easily scaleable.
A high efficiency RF plasma thruster comprising:
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