System and method of photoionization of fullerene and derivative clusters for high thrust-density ion thrusters
View Patent ↗The present invention is for a system and a method of VUV photoionization of fullerene and derivative clusters followed by their thermal effusion for a practical energy-efficient and economically-viable high thrust density ion thruster. By taking advantage of the state-of-the-art high intensity VUV photon sources, present invention is able to provide much softer ionization with minimal internal energy deposition than the ionization in the electron impact or charge exchange type ionization in plasma environment used in conventional ion thrusters. Because the invention eliminates the need of additional gas for forming discharge plasma, it permits simpler and lighter structures than the conventional fullerene thrusters with significantly enhanced propellant-usage efficiencies, thrust to power ratios, and thrust to weight ratios. Because the present invention employs softer VUV photoionization, it permits the usage of heavier and more complex fullerene derivatives, nanotubes, and nanotube derivatives than fullerene clusters for fuels without significantly fragmenting them.
1. A thruster comprising:
an effusion source comprising a heater assembly and an aperture, the heater assembly configured to heat a solid comprising fullerene to generate a jet that exits the aperture, the jet comprising vaporized fullerene and/or vaporized fullerene derivative clusters;
a photon source having a discharge chamber containing rare gases, the photon source configured to generate Vacuum Ultraviolet (VUV) photons to photionize the jet thereby creating a stream comprising fullerene ions;
the photon source further comprising a window which is VUV transparent, the photon source having a baffle system configured to block deposition of fullerene and fullerene derivative clusters on the window;
the photon source further comprising a first heater configured to clear deposits of fullerene and fullerene derivative clusters from the window;
an ion acceleration assembly comprising at least a first electrode downstream of the aperture and a second electrode downstream of the first electrode, the first and second electrodes being configured to accelerate the stream;
the ion acceleration assembly further comprising a second heater configured to evaporate deposits of fullerene and fullerene derivatives from the first and second electrodes.
2. A method of providing a thrust with the system of claim 1 , the method comprising the steps of;
evaporating the solid with the heater assembly thereby creating the jet;
generating VUV photons with the photon source thereby ionizing the jet and creating the stream;
accelerating the stream with the ion acceleration assembly thereby providing the thrust.
3. The method of claim 2 further comprising the step of, heating the first heater thereby clearing deposits of fullerene and fullerene derivative clusters from the window.
4. The method of claim 2 further comprising the step of, heating the second heater thereby clearing deposits of fullerene and fullerene derivative clusters from the first and second electrodes.