Predicate |
Object |
assignee |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_76ba102ea9c02b6633d64bf09c5b89a4 |
classificationCPCAdditional |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/H01Q9-30 |
classificationCPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64G1-66 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/H01Q1-288 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64G1-105 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/H01Q19-106 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64G1-222 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64G1-443 |
classificationIPCAdditional |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/H01Q9-30 |
classificationIPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B64G1-44 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/H01Q1-28 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/H01Q19-10 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B64G1-22 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B64G1-10 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B64G1-66 |
filingDate |
2013-06-11-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
grantDate |
2018-05-08-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
inventor |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_0d3768e138c064f94fbbaddee664b00b http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_4a8a8cfa7fca443f0f009ec79fe9d6a5 http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_ba39c9bb893f0c327a03578c089506be http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_11b1abbbb80708dcbb087176748453b4 |
publicationDate |
2018-05-08-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
publicationNumber |
US-9966658-B2 |
titleOfInvention |
Antennas for small satellites |
abstract |
Various embodiments of the present invention include assemblies and methods for utilizing antennas with high gain in small satellites. In one embodiment, a satellite comprising a payload configured for transmitting data is provided. The payload may include various components of the satellite, such as the attitude control system, electrical power system, and/or communication system. The satellite may be configured to communicate with one or more ground stations. The satellite includes a support structure comprising at least one deployable panel, wherein the support structure houses the payload. The satellite also includes at least one antenna coupled to the support structure, wherein the deployable panel is configured to cover the antenna in a non-deployed state and to expose the antenna in a deployed state. |
isCitedBy |
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-11502414-B2 http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-10917173-B2 http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-2020021361-A1 http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-11349558-B2 http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-11005165-B2 http://rdf.ncbi.nlm.nih.gov/pubchem/patent/WO-2021217215-A1 http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-2018076895-A1 http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-D989048-S http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-10897303-B1 http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-10530478-B2 |
priorityDate |
2012-06-11-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
type |
http://data.epo.org/linked-data/def/patent/Publication |