http://rdf.ncbi.nlm.nih.gov/pubchem/patent/JP-H1123196-A
Outgoing Links
| Predicate | Object |
|---|---|
| assignee | http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_f1192a135e4bc40a5f201a9646f20172 |
| classificationIPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F42B12-06 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F42B5-10 |
| filingDate | 1997-06-30-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| inventor | http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_05613678ccf397d55b3280052ea87a5f |
| publicationDate | 1999-01-26-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationNumber | JP-H1123196-A |
| titleOfInvention | Flying object |
| abstract | (57) [Summary] [PROBLEMS] To achieve a penetrator to a target with almost no need for trajectory control after achieving weight reduction and miniaturization. The solid propellant has a solid propellant, a nozzle, and a penetrator. The solid propellant is accelerated to an extremely high speed by the combustion of the solid propellant after being fired at an initial velocity from a low reaction launching device. When the combustion of the fuel cell 3 was completed, the penetrator 7 was made separable in the orbital direction. |
| isCitedBy | http://rdf.ncbi.nlm.nih.gov/pubchem/patent/FR-2821420-A1 |
| priorityDate | 1997-06-30-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| type | http://data.epo.org/linked-data/def/patent/Publication |
Incoming Links
Total number of triples: 23.