http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-2022194633-A1
Outgoing Links
| Predicate | Object |
|---|---|
| assignee | http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_728cbe1f705ae61501f25d61297d180c |
| classificationCPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F03H1-0037 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F03H1-0012 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64G1-405 |
| classificationIPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B64G1-40 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F03H1-00 |
| filingDate | 2021-12-10-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| inventor | http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_0fce13a6ca4d5a2297cf27d654604cbc http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_1dcba44f8fdaa88db49495cf4e6696c2 http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_44d6ae07a0c551b57c36b220483b5628 http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_bab64a61f269cf30bc21775d434f2188 http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_e6d5de8cb65948a4acbb4eadadf9d723 http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_f70eabc4eea2f7db22eb9f125be3488f |
| publicationDate | 2022-06-23-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationNumber | US-2022194633-A1 |
| titleOfInvention | Micro scalable thrusters for adaptive mission profiles in space - ustamps |
| abstract | One or more electrospray emitters form an electrospray thruster, suitable for generating thrust for maneuvering and/or moving a structure to which the thruster is attached in three-dimensional space. The thruster includes a reservoir containing a fluid, preferably an ionic liquid (IL) fluid. Each electrospray emitter includes a dielectric, with channel(s) formed through a thickness thereof, and an extraction electrode, preferably an extraction grid, on an opposite side of the dielectric from the reservoir. Upon application of a sufficient electric potential differential between the extraction electrode and the fluid, the fluid flows through the channels from the reservoir, forms a Taylor cone at an outlet of each channel, and is ejected in the direction of the extraction grid to generate a thrust by the thruster for movement and/or maneuvering of the structure to which the thruster is attached. |
| priorityDate | 2020-12-18-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| type | http://data.epo.org/linked-data/def/patent/Publication |
Incoming Links
Total number of triples: 23.