| Predicate |
Object |
| assignee |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_e83368888d58b13b931d0098d8f43c4d |
| classificationCPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F02K9-24
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F02K9-18
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F02K9-34 |
| classificationIPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F02K9-34
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F02K9-24
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F02K9-18 |
| filingDate |
1978-10-25-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| inventor |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_30bfbe0f7b110dbb7bda55a4c9f7e4a0
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_0eba91ab67c7d71145ff8ad58cd6e393 |
| publicationDate |
1986-03-07-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationNumber |
FR-2569773-A1 |
| titleOfInvention |
SOLID PROPERGOL FUSED MOTOR AND METHOD FOR MANUFACTURING THE SAME |
| abstract |
THE INVENTION RELATES TO A ROCKET ENGINE A SOLID PROPERGOL. IT CONTAINS A SOLID PROPERGOL I WHICH IS FLOWED DIRECTLY INTO A COMBUSTION CHAMBER EQUIPPED, AT ITS PIPE END, WITH AN INSULATING SLEEVE III. THIS ROCKET MOTOR ALLOWS THE BEST USE OF THE INTERIOR VOLUME OF THE COMBUSTION CHAMBER, WHEREAS THE POWER IS INCREASED. IT IS ALSO MUCH MORE CONVENIENT TO MANUFACTURE SINCE THE ESSENTIALS OF ISOLATION HAVE BEEN ABANDONED. |
| priorityDate |
1977-10-27-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| type |
http://data.epo.org/linked-data/def/patent/Publication |