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Solid Electrolyte-based Microthrusters
| Content Provider | The Lens |
|---|---|
| Abstract | A microthruster system may include a substrate and a source film. The substrate may include a plurality of emitter tips, and a source film deposited on the substrate. The source film may include silver. The microthruster system may also include a solid electrolyte film, which may include chalcogenide film, deposited over the source film. The solid electrolyte film may cause ions of the source film to move to the plurality of emitter tips. |
| Related Links | https://www.lens.org/lens/patent/012-625-319-004-894/frontpage |
| Language | English |
| Publisher Date | 2019-08-13 |
| Access Restriction | Open |
| Content Type | Text |
| Resource Type | Patent |
| Jurisdiction | United States of America |
| Date Applied | 2016-05-16 |
| Applicant | The United States of American As Represented By The Administrator of Nasa Us Administrator of The National Aeronautics and Space Administration |
| Application No. | 201615155574 |
| Claim | An apparatus, comprising: a substrate with a plurality of emitter tips; a source film, comprising silver or copper, deposited on the substrate; and a solid electrolyte film, comprising chalcogenide film, deposited over the source film, wherein the solid electrolyte film causes silver or copper ions within the source film to move towards the plurality of emitter tips. The apparatus of claim 1 , further comprising: a reservoir comprising silver or copper is used to supply the silver or copper ions from the source film to the plurality of emitter tips. The apparatus of claim 1 , wherein the source film is on top of the substrate, on bottom of the substrate, or both. The apparatus of claim 1 , wherein the substrate comprises a plurality of perforated holes. The apparatus of claim 4 , wherein each of the plurality of perforated holes is filled with silver or copper to allow the silver or copper ions to be transported up to the plurality of emitter tips, generating a silver or copper emission plume through an extractor grid. The apparatus of claim 1 , wherein the silver or copper ions move in response to an electric field, an electric chemical potential gradient, or both. The apparatus of claim 1 , wherein at least two of the plurality of emitter tips are identica A microthruster system, comprising: an electrolyte film coated on a solid metal film to move metal ions to a plurality of tips in the microthruster system, wherein the electrolyte film coated on the solid metal film creates a covalently bonded chalcogenide electrolyte film. The microthruster system of claim 8 , wherein the covalently bonded chalcogenide electrolyte film is vacuum compatible, and allows for transport of metal ions near room temperature, approaching liquid-like conductivities. The microthruster system of claim 8 , wherein the solid metal film comprises silver or copper. The microthruster system of claim 8 , further comprising: a solid metal reservoir connected to the solid metal film, and supplies the metal ions from the solid metal reservoir to the plurality of emitter tips. The microthruster system of claim 8 , wherein the solid metal film is on top of a substrate of the microthruster system, on bottom of the substrate of the microthruster system, or both. The microthruster system of claim 12 , wherein the substrate of the microthruster system comprises a plurality of perforated holes. The microthruster system of claim 13 , wherein each of the plurality of perforated holes is filled with metal to allow the metal ions to be transported to the plurality of emitter tips, generating an emission plume through an extractor grid. The apparatus of claim 8 , wherein the metal ions move in response to an electric field, an electric chemical potential gradient, or both. The microthruster system of claim 13 , wherein at least two of the plurality of emitter tips are identica A process for fabricating a microthruster system, comprising: depositing a solid metal film on a substrate of the microthruster system using thermal evaporation; depositing an electrolyte film on the solid metal film, wherein the depositing of the electrolyte film creates a covalently bonded chalcogenide electrolyte film to move metal ions within the solid metal film to a plurality of tips in the microthruster system. The process of claim 17 , wherein thermal evaporation is used to deposit the electrolyte film on the solid metal film. The process of claim 18 , wherein sputtering is used to deposit the electrolyte film on the solid metal film. The process of claim 17 , further comprising: photo-doping of the electrolyte film and the solid metal film by exposure to ultraviolet light. The apparatus of claim 1 , wherein at least two of the plurality of emitter tips vary in one or more of size and shape. The microthruster system of claim 13 , wherein at least two of the plurality of emitter tips vary in one or more of size and shape. |
| CPC Classification | PRODUCING A REACTIVE PROPULSIVE THRUST; NOT OTHERWISE PROVIDED FOR COATING METALLIC MATERIAL;COATING MATERIAL WITH METALLIC MATERIAL;SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE; BY CHEMICAL CONVERSION OR SUBSTITUTION;COATING BY VACUUM EVAPORATION; BY SPUTTERING; BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION; IN GENERAL COSMONAUTICS;VEHICLES OR EQUIPMENT THEREFOR |
| Examiner | Gerald L Sung William L Breazeal |
| Extended Family | 012-625-319-004-894 |
| Patent ID | 10378521 |
| Inventor/Author | West William C |
| IPC | F03H1/00 B64G1/40 C23C14/06 C23C14/14 C23C14/58 |
| Status | Inactive |
| Owner | California Institute of Technology United States of America As Represented By The Administrator of Nasa |
| Simple Family | 012-625-319-004-894 |
| CPC (with Group) | F03H1/0012 F03H1/005 C23C14/0623 C23C14/34 B64G1/413 C23C14/14 C23C14/5846 |
| Issuing Authority | United States Patent and Trademark Office (USPTO) |
| Kind | Patent/Patent 1st level of publication/Inventor's certificate |
