| Predicate |
Object |
| assignee |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_230c5c9d495e3bf392ef2b8098e51921 |
| classificationCPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C06B23-007
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C06B45-10 |
| classificationIPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C06B23-00
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C06B45-10 |
| filingDate |
1978-10-16-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| grantDate |
1980-07-01-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| inventor |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_4d34dee43238bfd69375987532227c10 |
| publicationDate |
1980-07-01-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationNumber |
US-4210474-A |
| titleOfInvention |
Silicone containing solid propellant |
| abstract |
Addition of a small amount, for example 1% by weight, of a liquid silicone oil to a metal containing solid rocket propellant provides a significant reduction in heat transfer to the inert nozzle walls eliminating metal oxide slag collection and blockage of the nozzle and increases burning rate by about 5 to 10% improving ballistic performance. |
| isCitedBy |
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-4412874-A
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-5554820-A
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/CN-108367997-A
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/WO-2017131841-A3
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-4332631-A
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/FR-2523954-A1
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-4953476-A |
| priorityDate |
1978-10-16-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| type |
http://data.epo.org/linked-data/def/patent/Publication |