Electrospray thruster with inverted geometry
View Patent ↗The present invention relates to electrospray thrusters, processes of making electrospray thrusters, and methods of using such electrospray thrusters. Applicant's thruster incorporates a unique geometry for the emitters and extractor grid that effectively eliminates ion interception on the grid, which is the primary failure mechanism of current devices, yet maintains the electric field conditions necessary for ion emission to occur. Without grid impingement, the thrust produced by the thruster is increased and thruster operational lifetime is increased substantially. Additionally, this non-traditional geometry also allows for higher electric fields at the emitter tip for a given applied voltage, thus enabling lower operational voltage of the thruster as compared to conventional designs.
1. An electrospray thruster, said electrospray thruster comprising:
a) an emitter array having a platform composed of emitters disposed on a surface of the platform, each emitter of the emitters having a respective body and a respective tip; and
b) an extractor grid having a lower surface, an upper surface and cylindrical apertures from said lower surface to said upper surface, said extractor grid being positioned such that each tip protrudes through a respective aperture among the cylindrical apertures so as to protrude past the lower surface and to protrude past the upper surface, and wherein each tip is centered in a respective aperture among the cylindrical apertures; and
a distance between said lower surface and said surface of the platform results in an arc index of zero or less.
2. The electrospray thruster according to claim 1 , wherein each tip protrudes through the respective aperture among the cylindrical apertures from 3 times a radius of curvature of each tip to 20 times the radius of curvature of each tip.
3. The electrospray thruster according to claim 2 , wherein each tip protrudes through the respective aperture among the cylindrical apertures from 5 times the radius of curvature of each tip to 15 times the radius of curvature of each tip.
4. The electrospray thruster according to claim 3 , wherein each tip protrudes through the respective aperture among the cylindrical apertures from 8 times the radius of curvature of each tip to 12 times the radius of curvature of each said tip.
5. The electrospray thruster according to claim 1 , wherein each body contains no features sharper than 5 times the radius of curvature of each respective tip.
6. The electrospray thruster according to claim 5 , wherein each body contains no features sharper than 10 times the radius of curvature of each respective tip.
7. The electrospray thruster according to claim 6 , wherein each body contains no features sharper than 20 times the radius of curvature of each respective tip.
8. The electrospray thruster according to claim 1 wherein each emitter of said emitters has a respective outer conical surface, each outer conical surface having a respective fixed, constant angle with respect to each respective tip.
9. The electrospray thruster according to claim 8 wherein each fixed constant angle deviates across said respective conical surface by no more than 6 degrees.
10. The electrospray thruster according to claim 9 wherein each fixed constant angle deviates across said respective conical surface by no more than 3 degrees.
11. The electrospray thruster according to claim 10 wherein each fixed constant angle deviates across said respective conical surface by no more than 1 degree.
12. The electrospray thruster according to claim 1 , wherein said emitters are staggered.
13. The electrospray thruster according to claim 1 , said emitter array has an emitter density of 2 emitters per square centimeter to 1100 emitters per square centimeter.
14. The electrospray thruster according to claim 1 , wherein said emitter array comprises a porous material.
15. The electrospray thruster according to claim 1 , wherein each tip is centered in the respective aperture among the cylindrical apertures such that a center position of each tip deviates no more than 100 microns from a true center of the respective aperture among the cylindrical apertures.
16. The electrospray thruster, according to claim 1 , said thruster comprising a thruster housing, a multi-component propellant module, said propellant module and said extractor grid sitting within said thruster housing, said extractor grid being positioned above said multi-component propellant module.
17. The electrospray thruster, according to claim 16 , wherein said thruster housing is adjustable:
a) to set a tip protrusion distance through said cylindrical apertures; and/or
b) to set tip centering in said cylindrical apertures.
18. A space vehicle comprising an electrospray thruster according to claim 1 .
19. A process for making an electrospray thruster, said process comprising assembling the electrospray thruster comprising:
a) an emitter array having a platform composed of emitters disposed on a surface of the platform, each emitter of the emitters having a respective body and a respective tip; and
b) an extractor grid having a lower surface, an upper surface and cylindrical apertures from said lower surface to said upper surface, said extractor grid being positioned such that each tip protrudes through a respective aperture among the cylindrical apertures so as to protrude past the lower surface and to protrude past the upper surface, and wherein each tip is centered in the respective cylindrical aperture among the cylindrical apertures, and a distance between said lower surface and said surface of the platform results in an arc index of zero or less.
20. A process according to claim 19 wherein each tip is centered in the respective aperture among the cylindrical apertures such that a respective center position of each tip deviates no more than 100 microns from a respective true center of said respective aperture.