http://rdf.ncbi.nlm.nih.gov/pubchem/patent/JP-H05270963-A
Outgoing Links
| Predicate | Object |
|---|---|
| classificationCPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C06B45-10 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C06B33-04 |
| classificationIPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C06B33-04 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C06B45-10 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C06D5-06 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C06D5-00 |
| filingDate | 1992-12-28-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationDate | 1993-10-19-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationNumber | JP-H05270963-A |
| titleOfInvention | Stable solid rocket propellant composition |
| abstract | (57) Summary [Objective] The present invention provides a stable chlorine-free solid rocket propellant composition. The chlorine-free stable solid rocket propellant composition according to the present invention comprises (A) a low energy binder component having an explosion heat value not exceeding about 350 cal / g, wherein the binder component is (a) A polyether-based or polyester-based polymer; and (b) at least one high energy plasticizer; (B) nitrate and / or phase stabilizing nitrate as an oxidant component; (C) Mg as a fuel component / Al alloy, then M The content of g is limited; and (D) a catalyst for controlling the burning rate. |
| isCitedBy | http://rdf.ncbi.nlm.nih.gov/pubchem/patent/JP-4621474-B2 http://rdf.ncbi.nlm.nih.gov/pubchem/patent/JP-2006117444-A http://rdf.ncbi.nlm.nih.gov/pubchem/patent/JP-2006225253-A |
| priorityDate | 1991-12-27-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| type | http://data.epo.org/linked-data/def/patent/Publication |
Incoming Links
Total number of triples: 82.