| Predicate |
Object |
| assignee |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_8d5a341eef325eacc41deb3bcc9fa1bb
http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_bd587677e8c76f913ce75390bb6b83ac |
| classificationCPCAdditional |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C10G2400-08
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C10G2300-301 |
| classificationCPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C10G35-095
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C06B25-20
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F02K9-42
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C10L1-04 |
| classificationIPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C10L1-04 |
| filingDate |
2013-03-25-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| inventor |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_4b8a0887be8e82377d96de686c829fe0 |
| publicationDate |
2014-04-03-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationNumber |
WO-2014011250-A3 |
| titleOfInvention |
High performance liquid rocket propellant |
| abstract |
Disclosed is a high performance hydrocarbon fuel characterized by a hydrogen content greater than 14.3% by weight, a hydrogen to carbon atomic ratio greater than 2.0 and/or a heat of combustion greater than 18.7 KBtu/lb. The disclosed fuels generally have a paraffin content that is at least 90% by mass and a C 12 -C 20 isoparaffin content of at least 40% by mass. |
| priorityDate |
2012-03-23-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| type |
http://data.epo.org/linked-data/def/patent/Publication |