http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-7966805-B2
Outgoing Links
| Predicate | Object |
|---|---|
| assignee | http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_b5231c81de1a546c1d6a9325c10910ce |
| classificationCPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F02K9-72 |
| classificationIPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C06D5-04 |
| filingDate | 2007-05-15^^<http://www.w3.org/2001/XMLSchema#date> |
| grantDate | 2011-06-28^^<http://www.w3.org/2001/XMLSchema#date> |
| inventor | http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_66b06f274d459e1181e93ba5af39c520 |
| publicationDate | 2011-06-28^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationNumber | US-7966805-B2 |
| titleOfInvention | Hydroxyl amine based staged combustion hybrid rocket motor |
| abstract | A new rocket motor assembly configuration is disclosed. Amine based oxidizer is decomposed in the presence of a metallic catalyst to generate an oxygen rich hot gas stream. The hot gas stream is used to trigger a Magnesium based solid fuel in the combustion chamber. The thrust of the rocket motor may be regulated at multiple points. This design thus offers an IM compliant, thrust-adjustable rocket motor that is of a low hazard classification without compromising its performance. |
| isCitedBy | http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-9151579-B2 http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-2010242772-A1 |
| priorityDate | 2007-05-15^^<http://www.w3.org/2001/XMLSchema#date> |
| type | http://data.epo.org/linked-data/def/patent/Publication |
Incoming Links
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