http://rdf.ncbi.nlm.nih.gov/pubchem/patent/UA-53630-U
Outgoing Links
Predicate | Object |
---|---|
assignee | http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_971ee4d39641a5a9464b718d45215a4f |
classificationIPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F03H1-00 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F03H3-00 |
filingDate | 2010-04-26-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
inventor | http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_a002eb7947d2c6894cdb5319b9e97c6b |
publicationDate | 2010-10-11-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
publicationNumber | UA-53630-U |
titleOfInvention | PHOTON-Plasma Rocket Engine |
abstract | Photon-plasma rocket engine consists of a power supply system, control system, ignition system, liquid lithium tank, magnetic plasma ionization coil, magnetic plasma heating coil, magnetic nozzle, Mach probe, Langmuir probe, pressure gauges in the system as well as a vacuum chamber and thermocouple. The engine includes laser traps that contain antihydrogen and deuterium (tanks), laser accelerators that accelerate the antihydrogen and deuterium to energy of 2 GeV for their more efficient interaction. In their interaction, two gamma-ray quanta with an energy of 0.93 GeV and pi-mesons are released, which interact with the walls of the tungsten reflector of the annihilation reactor and thus generate pairs of positrons and electrons in the field of tungsten nuclei and in the field of tungsten atomic electrons, as well as quanta that penetrate the reactor wall and ionize lithium, which is heated to the liquid state by thermoelectric heaters in the tank, and the ionized lithium due to cyclotron resonance is heated to the plasma and accelerated to a predetermined the ranks. The solenoid valve, which is coupled to thermocouples and pressure gauges through the control system, regulates the supply of liquid lithium to the cooling system of the annihilation reactor, and the total propulsion force of the rocket engine consists of the leakage of lithium ions, ray energy of gamma quanta and pyum quantum rays. [Photon-plasma rocket engine consists of a power system, control system, ignition system, liquid lithium tank, magnetic plasma ionization coil, magnetic plasma heating coil, magnetic nozzle, |
priorityDate | 2010-04-26-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
type | http://data.epo.org/linked-data/def/patent/Publication |
Incoming Links
Total number of triples: 17.