http://rdf.ncbi.nlm.nih.gov/pubchem/patent/KR-20190043294-A
Outgoing Links
| Predicate | Object |
|---|---|
| assignee | http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_51f0be568b420c681d28154f6594bb6b |
| classificationCPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F42B10-38 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F42B10-34 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F02K7-105 |
| classificationIPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F02K7-10 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F42B10-38 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F42B10-34 |
| filingDate | 2017-10-18-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| inventor | http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_5a6e12bdec9195e5d84e714d0122d37f http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_652317452802dc84afd1b2ec4dcb82e7 http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_ba3654aebf73555f57763c949a71a3c5 http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_85a1642f644b774807cb4f7888ea2cb9 http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_d0cc29e647ac0e232937ca473a37e51c |
| publicationDate | 2019-04-26-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationNumber | KR-20190043294-A |
| titleOfInvention | Ramjet Solid Fuel with Ignition Support for Gun-Propelled Ramjet Shell |
| abstract | In order to extend the range of 105 mm, 155 mm, 8 inch, or 3 inch, 5 inch hammer shells that are launched to support firepower, The present invention relates to a ramjet fuel which is applied to a range-extended gun mounted with a ramjet engine, which allows a ramjet engine to operate quickly by applying an ignition auxiliary means to the fuel, 1. A ramjet solid fuel which is applied to a range extension gun mounted with a ramjet engine so as to extend the range of the cannon and is disposed between the intake port of the ramjet engine and the injection nozzle, comprising: a fuel body 10 of annular solid; An ignition auxiliary material (20) applied to the fuel body (10) to ignite the fuel body, the fuel body (10) comprising 40 to 90 wt% of HTPB fuel; 5-15 wt% AP oxidizer; 5 to 15 wt% of first metal particles made of aluminum (Al) or magnesium (Mg), and at least one metal selected from the group consisting of boron (B), boron carbide (B 4 C), zirconium (Zr), and zirconium carbide 0 to 30 wt% of the second metal particles; And inevitable impurities. |
| priorityDate | 2017-10-18-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| type | http://data.epo.org/linked-data/def/patent/Publication |
Incoming Links
Total number of triples: 46.