http://rdf.ncbi.nlm.nih.gov/pubchem/patent/RU-2171914-C1
Outgoing Links
| Predicate | Object |
|---|---|
| classificationIPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F03H99-00 |
| filingDate | 1999-11-29-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| grantDate | 2001-08-10-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationDate | 2001-08-10-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationNumber | RU-2171914-C1 |
| titleOfInvention | Thermonuclear space engine |
| abstract | FIELD: space engineering. SUBSTANCE: proposed thermonuclear space engine using for its operation energy of thermonuclear synthesis consists of microthermonuclear reactor with dc electric generator, tank with hydrogen, central and ionic channels enclosed by solenoid coils, ring-shaped cathode and anode of acceleration zone terminating in thrust nozzle. EFFECT: provision of speed in space up to 2•10 8 m/s.. 1 dwg |
| priorityDate | 1999-11-29-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| type | http://data.epo.org/linked-data/def/patent/Publication |
Incoming Links
Total number of triples: 28.