http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-2019390996-A1
Outgoing Links
| Predicate | Object |
|---|---|
| assignee | http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_f3272933112a9429eab53ca489f5ec69 |
| classificationCPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/G01F23-247 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64G1-402 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F17C13-008 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F17C13-026 |
| classificationIPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B64G1-40 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/G01F23-24 |
| filingDate | 2017-12-08-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| inventor | http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_4e8580f481bc934acb34e113be440f27 http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_314b7bef7a41f9c07b74463eb275ce49 http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_1a4fa24195e77ef573dbcd74f7e7fe1c http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_ad30b417a7b08bdd74959ec7ac791968 |
| publicationDate | 2019-12-26-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationNumber | US-2019390996-A1 |
| titleOfInvention | Method for thermally gauging the tank of a spacecraft and a spacecraft equipped with means for implementing such a method |
| abstract | Disclosed is a method for gauging the liquid propellant tank of a spacecraft during a phase of high-thrust along an axis, the tank being thermally conductive and having a known geometry. The method includes steps of: attaching, on a wall of the tank, a heating member and at least one temperature sensor in proximity to the heating member and in a plane of interest perpendicular to the thrust axis; during the high-thrust phase, heating the wall of the tank and acquiring temperature measurements of the wall of the tank at rapid frequency; determining the instant I when the temperature measured by the sensor changes, such change indicating the presence of the liquid-gas interface in the tank in the plane of interest; and determining the volume of liquid propellant present in the tank at instant I. |
| isCitedBy | http://rdf.ncbi.nlm.nih.gov/pubchem/patent/CN-114237040-A http://rdf.ncbi.nlm.nih.gov/pubchem/patent/CN-112629611-A |
| priorityDate | 2016-12-09-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| type | http://data.epo.org/linked-data/def/patent/Publication |
Incoming Links
| Predicate | Subject |
|---|---|
| isDiscussedBy | http://rdf.ncbi.nlm.nih.gov/pubchem/substance/SID419527398 http://rdf.ncbi.nlm.nih.gov/pubchem/compound/CID25352 |
Total number of triples: 22.