http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-2021355046-A9

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classificationCPCInventive http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C06B47-02
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http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C06B47-00
classificationIPCInventive http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C06B47-00
filingDate 2020-07-02-04:00^^<http://www.w3.org/2001/XMLSchema#date>
inventor http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_6e3448804cfe311b9d92b27f1018065c
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_09cc5359197aaa28bf9e00a17811a614
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publicationDate 2021-11-18-04:00^^<http://www.w3.org/2001/XMLSchema#date>
publicationNumber US-2021355046-A9
titleOfInvention Hypergolic two-component system for rocket engines
abstract The present invention relates to a hypergolic two-component system for rocket engines, including a fuel and an oxidising agent provided in a manner separated from one another and can be reacted in a rocket engine by bringing them into contact with one another. The fuel is an ionic liquid comprising a thiocyanate anion and one or more cations. The cation or cations are selected from one or more imidazolium ions of the general formula I, triazolium ions of the general formula II or III, and/or tetrazolium ions of the general formula IV, where R 1 is a C 1 - to C 6 -alkyl radical or a C 2 - to C 6 -alkenyl radical, where R 2 is hydrogen or a C 1 - to C 6 -alkyl radical or a C 2 - to C 6 -alkenyl radical, and where X 1 , X 2 and X 3 are each independently hydrogen, a C 1 - to C 6 -alkyl radical or a C 2 - to C 6 -alkenyl radical, and the oxidising agent comprises hydrogen peroxide.
priorityDate 2019-07-19-04:00^^<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: 52.