http://rdf.ncbi.nlm.nih.gov/pubchem/patent/RU-2147344-C1
Outgoing Links
Predicate | Object |
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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 |
Incoming Links
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