http://rdf.ncbi.nlm.nih.gov/pubchem/patent/KR-20200109898-A
Outgoing Links
| Predicate | Object |
|---|---|
| assignee | http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_3f405a4cd9405ab53cc2977c00c1e142 |
| classificationCPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C06B45-10 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F02K9-97 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F02K9-34 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C06D5-06 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F02K9-08 |
| classificationIPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F02K9-97 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C06D5-06 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C06B45-10 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F02K9-34 |
| filingDate | 2019-03-15^^<http://www.w3.org/2001/XMLSchema#date> |
| inventor | http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_b9f758b2a44e409d7c6448fb58207363 |
| publicationDate | 2020-09-23^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationNumber | KR-20200109898-A |
| titleOfInvention | Mass fraction controlled solid propellant |
| abstract | As the mass fraction of the solid propellant according to the present invention is controlled to fit the required thrust pile, it is possible to generate thrust over time, suitable for the surrounding environment of the projectile, and during the generation of thrust, the solid propellant Only combustion has the effect of having the desired thrust profile automatically. In addition, the solid propellant according to the present invention There is an effect that the controllable thrust range is remarkably increased, and the thrust change according to the combustion time can be immediately given, that is, it has the effect of having a continuous thrust change that can generate various thrusts over time. . |
| priorityDate | 2019-03-15^^<http://www.w3.org/2001/XMLSchema#date> |
| type | http://data.epo.org/linked-data/def/patent/Publication |
Incoming Links
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