http://rdf.ncbi.nlm.nih.gov/pubchem/patent/RU-2259495-C2
Outgoing Links
| Predicate | Object |
|---|---|
| classificationIPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F02K9-10 |
| filingDate | 2003-10-16-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| grantDate | 2005-08-27-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| inventor | http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_6f575bca94ab135d6d85e6c3b83e1983 http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_dcf19f101d6e054ceb293f5b6bad04dc http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_87f97b0430ea361d3539fe1528948881 http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_89fcc63b1f48a5cbd329c0c64b37466f http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_954d8b6f816edf1620c9ab2aa5d10550 http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_8408fbe86cefc82638528591acc6125d http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_3d0a7d83526397d3e71402eccf95a497 http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_774a3626c481af487850705a3978cf0f http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_1fd51d17494a3c26e11848d76fe7988b |
| publicationDate | 2005-08-27-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationNumber | RU-2259495-C2 |
| titleOfInvention | Solid-propellant charge |
| abstract | FIELD: rocketry. n SUBSTANCE: proposed solid-propellant charge consists of solid-propellant grain restricted along side surface and end face with cellulose acetate-based inhibitory coating with synthetic glue-based sheathing film layer applied over inhibitory coating. Through central channel is made in charge. Surface of central though channel made in charge is restricted together with side surface and front end face of charge with possibility of removal of part inhibitory coating from side of burning eng face of side surface. Ratio of diameter of solid-propellant grain (D) and diameter of channel (d) is 2.0<D/d<5.0. n EFFECT: reduced smoking, increased destructive effect of cumulative warhead of shell, optimum conditions of realization of cruise and acceleration and cruise operating conditions of rocket engine. n 3 cl, 2 dwg |
| isCitedBy | http://rdf.ncbi.nlm.nih.gov/pubchem/patent/RU-2533637-C2 http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-9291410-B2 |
| priorityDate | 2003-10-16-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| type | http://data.epo.org/linked-data/def/patent/Publication |
Incoming Links
| Predicate | Subject |
|---|---|
| isDiscussedBy | http://rdf.ncbi.nlm.nih.gov/pubchem/compound/CID8039 http://rdf.ncbi.nlm.nih.gov/pubchem/substance/SID410441611 |
Total number of triples: 22.