http://rdf.ncbi.nlm.nih.gov/pubchem/patent/FR-2655722-A1
Outgoing Links
| Predicate | Object |
|---|---|
| assignee | http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_20e54c0c349a380bf8764c1957728fd8 |
| classificationCPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F42B10-62 |
| classificationIPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F42B10-62 |
| filingDate | 1989-12-12-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| inventor | http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_91429a21cf5c5f244e5e6800d52520e7 |
| publicationDate | 1991-06-14-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationNumber | FR-2655722-A1 |
| titleOfInvention | SUPERSONIC MISSILE WITH TORQUE DRIVING BY SPOUILERS. |
| abstract | Supersonic guided missile, comprising a fuselage (2, 2 ', 2 ") terminated at the front by a nose (3, 3', 3") and at the rear by a base (4, 4 ', 4 ") , and provided on the outside with fixed rear stabilizers (5, 5 ', 5 "), characterized in that it comprises, longitudinally at a distance from the center of gravity (G1) at least one flap (7, 7', 7") movable, called a spoiler, between a hidden configuration inside the fuselage and an active configuration deployed transversely in which this flap projects laterally with respect to this fuselage. |
| priorityDate | 1989-12-12-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| type | http://data.epo.org/linked-data/def/patent/Publication |
Incoming Links
Total number of triples: 17.