Predicate |
Object |
assignee |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_fa7926dbf40ad24cefdb69cc6144d19d |
classificationCPCAdditional |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/Y10S149-124 |
classificationCPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C06B21-0091 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C06B45-10 |
classificationIPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C06D5-00 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C06B21-00 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C06B45-10 |
filingDate |
2000-12-06-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
inventor |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_2c267c13639844e4a5a49f4d9b3e2c77 http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_f21c2077b89319e6a73fe06e9b0d8323 |
publicationDate |
2002-03-14-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
publicationNumber |
US-2002029829-A1 |
titleOfInvention |
Solid rocket propellant |
abstract |
A solid rocket propellant includes a hydroxy-terminated caprolactone ether binder and an oxidizer. The propellant may be disposed of by contacting it with an aqueous solution of 12 N NaOH or 6 N HCI at a temperature of about 140° F. for about 24 hours to decompose the binder. Solids remaining in the solution after the binder decomposes are removed. |
isCitedBy |
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-8683933-B1 http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-9102575-B2 http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-2014082908-A1 |
priorityDate |
1999-07-16-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
type |
http://data.epo.org/linked-data/def/patent/Publication |