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classificationCPCInventive http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/H01S3-083
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/G01C19-668
classificationIPCInventive http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/H01S3-083
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/G01C19-66
filingDate 1992-05-29-04:00^^<http://www.w3.org/2001/XMLSchema#date>
grantDate 1993-11-09-04:00^^<http://www.w3.org/2001/XMLSchema#date>
inventor http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_2b310df5655d603cba1f15d6f2c1c64b
publicationDate 1993-11-09-04:00^^<http://www.w3.org/2001/XMLSchema#date>
publicationNumber US-5260962-A
titleOfInvention Compact Lightweight ring laser gyro
abstract A lightweight ring laser gyro (RLG) for vehicles including space vehicles is provided wherein the housing of such RLG, instead of being made of relatively heavy ULE glass, is made of low density silica aerogel having a density of from 600 to 1000 mg/cc. Further, where the prior art RLGs have three laser triangles, each mounted in one of three blocks, which blocks are mounted on separate orthogonal sides of a housing, the RLG of the present invention employs but one block with all three laser triangles orthogonally machined therein for a considerable size reduction or compactness and a further weight savings. The RLG of the invention can be attached to, e.g. space vehicles, including satellites for guidance and monitoring thereof. Also, the substrates of mirrors mounted on such RLG can also be made of LD aerogels for a further weight savings not seen in the prior art.
isCitedBy http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-2008002208-A1
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priorityDate 1992-05-29-04:00^^<http://www.w3.org/2001/XMLSchema#date>
type http://data.epo.org/linked-data/def/patent/Publication

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Total number of triples: 43.