http://rdf.ncbi.nlm.nih.gov/pubchem/patent/JP-H05310491-A
Outgoing Links
Predicate | Object |
---|---|
assignee | http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_2f8cfa5aee4410611b5c562275c9f8e3 http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_b3b275afa0850f4e61db127b41613765 |
classificationIPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C06D5-00 |
filingDate | 1992-05-08-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
inventor | http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_f2b82e42d88e63994ec665a8f8e0a2d9 http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_241138d993b29067bb7aaa3a76aac31a http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_2f0f003649c62357039cd665cf6eea0b |
publicationDate | 1993-11-22-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
publicationNumber | JP-H05310491-A |
titleOfInvention | Composite propellant composition |
abstract | (57) [Summary] [Purpose] To provide a propellant having excellent combustion performance and mechanical properties. [Structure] In a composite propellant composition containing an oxidizing agent and a binder as essential components, the main component of the binder is a terminal hydroxyl group azide polymer represented by the general formula (I). [Chemical 1] (In the formula, n and m represent positive numbers.) |
priorityDate | 1992-05-08-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
type | http://data.epo.org/linked-data/def/patent/Publication |
Incoming Links
Total number of triples: 50.