http://rdf.ncbi.nlm.nih.gov/pubchem/patent/RU-2147344-C1

Outgoing Links

Predicate Object
assignee http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_5da8574a57f79f1f1fc3710d256f0e95
http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_b3a9ce8af52df230b2b1ad03428ff8bf
classificationIPCInventive http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F02K9-50
filingDate 1998-08-20^^<http://www.w3.org/2001/XMLSchema#date>
grantDate 2000-04-10^^<http://www.w3.org/2001/XMLSchema#date>
inventor http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_9544f6e02acc70dbc724232484eaff67
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_0c3142e9cc7858fce9742c9687cd0cc2
publicationDate 2000-04-10^^<http://www.w3.org/2001/XMLSchema#date>
publicationNumber RU-2147344-C1
titleOfInvention Fuel and oxidizer tank pressurization system of spacecraft engine plant
abstract FIELD: jet engine plants of spacecraft. SUBSTANCE: proposed system includes high-pressure gas sources communicated with gas cavities of fuel and oxidizer propellant tanks by means of pneumatic lines, start and cut-off valves and gas reducers. Used as high-pressure gas source is tetra ammoniate of boron of aluminum or diammoniate of boron hydride of zinc made in form of grains having thermal contact with heaters and placed in hermetic containers. EFFECT: improved mass and dimensional characteristics due to making use of properties of some solid materials of releasing great amount of gas at heating through thermochemical reaction. 1 dwg
isCitedBy http://rdf.ncbi.nlm.nih.gov/pubchem/patent/RU-2582372-C2
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/WO-2012172238-A1
priorityDate 1998-08-20^^<http://www.w3.org/2001/XMLSchema#date>
type http://data.epo.org/linked-data/def/patent/Publication

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