http://rdf.ncbi.nlm.nih.gov/pubchem/patent/JP-H09151798-A

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Predicate Object
assignee http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_74973199515dbabd2310245aab03e282
http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_db024f0651fab7a935373a4e9a79c185
classificationIPCInventive http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F02K9-52
filingDate 1995-11-29^^<http://www.w3.org/2001/XMLSchema#date>
inventor http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_6a9e0c4833396cb15de00d71d28243e5
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_34ff6eea84871f4757e19d8b890183e9
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_5f663d45cd40cab887a1564c5b92d820
publicationDate 1997-06-10^^<http://www.w3.org/2001/XMLSchema#date>
publicationNumber JP-H09151798-A
titleOfInvention Rocket engine injectors
abstract (57) Abstract: Even if the combustion pressure or the mixing ratio of the liquid oxidizer and the gas fuel is changed to change the thrust of the rocket engine, the gas fuel and the liquid oxidizer injected from the injector into the combustion chamber are changed. Improves rocket performance by maintaining jet velocity at a reasonable value. An injector of a rocket configured to inject into a combustion chamber a gas fuel 1 flowing around a liquid oxidizer 2 injected into the combustion chamber of the rocket and flowing through a cooling passage of a combustion chamber and a rocket nozzle. The portion 3a of the outer wall 3 forming the injection hole is made of a shape memory alloy that deforms so as to reduce the injection hole during high pressure combustion. Also, the portion 3a Was composed of a shape memory alloy that deforms so as to reduce the injection holes when the mixing ratio of the liquid oxidizer and the gas fuel is high.
isCitedBy http://rdf.ncbi.nlm.nih.gov/pubchem/patent/JP-2010503793-A
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/KR-100470278-B1
priorityDate 1995-11-29^^<http://www.w3.org/2001/XMLSchema#date>
type http://data.epo.org/linked-data/def/patent/Publication

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