http://rdf.ncbi.nlm.nih.gov/pubchem/patent/RU-2569658-C2

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filingDate 2014-02-26-04:00^^<http://www.w3.org/2001/XMLSchema#date>
grantDate 2015-11-27-04:00^^<http://www.w3.org/2001/XMLSchema#date>
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publicationDate 2015-11-27-04:00^^<http://www.w3.org/2001/XMLSchema#date>
publicationNumber RU-2569658-C2
titleOfInvention Space platform
abstract FIELD: aircraft engineering. n SUBSTANCE: space platform comprises module of service systems shaped to parallelepiped, assemblies of coupling with separation system, engine unit, solar cells and thermal control system. Space platform comprises cylindrical compartment composed of grate-like structure of black-reinforced plastic and cellular cells with supports. Said cylindrical compartment houses the tanks with working fluid for engine unit of correction system with plasma engine running on xenon and engine units of orientation and stabilisation system. n EFFECT: compact design, accelerated production of spacecraft based on this platform. n 4 dwg, 4 cl
isCitedBy http://rdf.ncbi.nlm.nih.gov/pubchem/patent/EA-035209-B1
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/RU-2624764-C1
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http://rdf.ncbi.nlm.nih.gov/pubchem/patent/RU-2617161-C1
priorityDate 2014-02-26-04:00^^<http://www.w3.org/2001/XMLSchema#date>
type http://data.epo.org/linked-data/def/patent/Publication

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Total number of triples: 25.