http://rdf.ncbi.nlm.nih.gov/pubchem/patent/GB-1161126-A
Outgoing Links
| Predicate | Object |
|---|---|
| assignee | http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_66e061087b8b0ca4bda35df8e395be73 |
| classificationCPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C06B45-10 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C06B45-12 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F42B1-00 |
| classificationIPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C06B45-12 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C06B45-10 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F42B1-00 |
| filingDate | 1966-08-10-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationDate | 1969-08-13-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationNumber | GB-1161126-A |
| titleOfInvention | Solid Propellant Inhibitor. |
| abstract | 1,161,126. Propellants. UNITED STATES OF AMERICA, ARMY, SECRETARY OF THE. 10 Aug., 1966 [10 Feb., 1966], No. 35748/66. Heading F3A. [Also in Division C3] A granular solid propellant, e.g. having the shape of a torroid, is inhibited by application of a composition comprising 80-90% by wt. of hydroxy terminated poly-butadiene, 2- 10% organic diisocyanate, e.g. hexamethylene or toluene diisocyanate, 1-15% of silica, carbon black or asbestos and at least 0À04% of ferric oxide, lead stannate, red lead or ferric acetyl acetonate. In the example the propellants used were of the double-base type and some contained aluminium metal and ammonium perchlorate. |
| priorityDate | 1966-02-10-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| type | http://data.epo.org/linked-data/def/patent/Publication |
Incoming Links
Total number of triples: 30.