| Predicate |
Object |
| assignee |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_727dd58746d791c09f47b3b6e5fd5e4c |
| classificationCPCAdditional |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/Y02E30-10 |
| classificationIPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F03H99-00
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/G21B1-00 |
| filingDate |
2015-04-03-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| inventor |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_080d4c288984d5a61082538a374742c2 |
| publicationDate |
2016-11-24-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationNumber |
JP-2016196872-A |
| titleOfInvention |
Fusion rocket engine |
| abstract |
An object of the present invention is to manufacture a fusion rocket engine using muon-catalyzed cold fusion. SOLUTION: Tritium and deuterium are burned with brown gas, and the energy of fusion is used as a driving force. [Selection] Figure 1 |
| priorityDate |
2015-04-03-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| type |
http://data.epo.org/linked-data/def/patent/Publication |