| Predicate |
Object |
| assignee |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_1d48c19432c7b8bb43d0f1ed50ab7fd9 |
| classificationCPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C06D5-10
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C06B45-10
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C08F265-06
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C08F279-02 |
| classificationIPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C08F265-06
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C06D5-10
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C06B45-10
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C08F279-02 |
| filingDate |
1972-05-12^^<http://www.w3.org/2001/XMLSchema#date> |
| grantDate |
1974-02-12^^<http://www.w3.org/2001/XMLSchema#date> |
| inventor |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_9a7c45988b847e92735f307d61a8e79f
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_c467f4647efbfa959a38f01c7401c5a4 |
| publicationDate |
1974-02-12^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationNumber |
US-3791140-A |
| titleOfInvention |
Operation of hybrid rocket systems |
| abstract |
In the operation of a hybrid rocket system, a solid fuel consisting essentially of a polybutadiene, trimethylolpropane trimethacrylate, polymethylmethacrylate and an organic peroxide is burned in a combustion zone in the presence of an oxidizer that is supplied to the zone at varying flow rates. Because the solid fuel burns without char formation at low oxidizer to fuel ratios, it is possible to operate the system over a wide thrust range. |
| isCitedBy |
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-5085717-A
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/DE-102010000261-B4
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/DE-102010000261-A1
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-5765361-A |
| priorityDate |
1972-05-12^^<http://www.w3.org/2001/XMLSchema#date> |
| type |
http://data.epo.org/linked-data/def/patent/Publication |