http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-11067064-B2

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classificationCPCInventive 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/F03H1-00
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B64G1-40
filingDate 2018-02-26-04:00^^<http://www.w3.org/2001/XMLSchema#date>
grantDate 2021-07-20-04:00^^<http://www.w3.org/2001/XMLSchema#date>
inventor http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_1ed90a090773ab5710177f06d061ac31
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_50c123a4bb152149eb088c98f95edaa9
publicationDate 2021-07-20-04:00^^<http://www.w3.org/2001/XMLSchema#date>
publicationNumber US-11067064-B2
titleOfInvention Propulsion systems including a sublimable barrier
abstract The present disclosure is related to propulsion systems (e.g., electrospray devices such as electrospray emitters and/or electrospray thrusters) having a sublimable barrier that may act as a passive valve for a propellant (e.g., a source of ions). The sublimable barrier may be located and arranged such that it physically separates a propellant, such as a source of ions, from an ambient environment exterior to the propulsion system. After the sublimable barrier has sublimated due to exposure to vacuum, and where appropriate diffused out of the propulsion system, the propulsion system may be operated normally. In some embodiments, the sublimable barrier may be a solid sublimable organic compound.
priorityDate 2018-02-26-04:00^^<http://www.w3.org/2001/XMLSchema#date>
type http://data.epo.org/linked-data/def/patent/Publication

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