| Predicate |
Object |
| assignee |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_926514a4805716ff3f04fdc6f91ab292 |
| classificationCPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C06B43-00 |
| classificationIPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C06B43-00 |
| filingDate |
1965-09-23-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| grantDate |
1973-07-24-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| inventor |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_6bb2329336287d1fccb1e79a607f2339
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_f4227186469618a5a5e031a9e0df9db1 |
| publicationDate |
1973-07-24-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationNumber |
US-3748199-A |
| titleOfInvention |
Composite propellants containing hydroxylammonium perchlorate |
| abstract |
A castable propellant composition including suitable curing agent(s) and a curable fuel binder(s) having a novel oxidizer, hydroxylammonium perchlorate. Optional propellant adjuvants are also disclosed for improving and/or increasing various propellant physical and chemical combustion characteristics. |
| isCitedBy |
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-4428785-A
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-4411717-A
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-4120709-A
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-5882545-A
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-6264896-B1
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-5574248-A
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-6126854-A
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-3986906-A
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-4377678-A
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-5627339-A
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-5623120-A |
| priorityDate |
1965-09-23-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| type |
http://data.epo.org/linked-data/def/patent/Publication |