ELECTROSTATIC PLASMA ENGINE OF A SPACE VEHICLE DRIVEN BY CHARGED PARTICLES FOR OPERATION IN SPACE Russian patent published in 2021 - IPC F03H1/00 

Abstract RU 2762764 C1

EFFECT: space technology.

SUBSTANCE: invention relates to the field of rocket and space equipment and can be used in space for interorbital tugs and long-term space interplanetary flights. The engine comprises a body, an evaporation chamber with a working substance, located in the body, a high-temperature source for decomposition of the working substance to the atomic level and formation of solid nano- and microparticles, a charging chamber, and an accelerating apparatus abutting thereon from the end, located wherein is an electrode system wherein the first electrode has a negative electric potential and is placed at the input of the accelerating apparatus, and the second electrode with a positive potential is placed at the output thereof, wherein the electrodes are placed at a distance from each other excluding an electric breakdown between the electrodes. The electrodes of the accelerating apparatus are connected to an external high-voltage current source in order to create a difference in the electrical potentials between the electrodes, providing a flow of charged nano- and microparticles flowing into the environment and thereby creating reactive thrust of the engine. Small-sized basalt soils taken from the surface of cosmic bodies, e.g., asteroids, sufficient in space, are used in the engine as a working material. The charging chamber is made in the form of a cavity placed between the inner wall of the engine housing and the outer wall of the evaporation chamber, wherein electric heaters providing heat emission of electrons for charging solid nano- and microparticles are placed inside the charging chamber.

EFFECT: proposed structure of an engine and application of new working materials as fuel will allow for practical implementation of long-term flights in space.

8 cl, 1 dwg

Similar patents RU2762764C1

Title Year Author Number
TWO-REGIME ROCKET ENGINE 1994
  • Bajsiev Khadzhi-Murat Khasanovich
RU2084676C1
ELECTRIC PRIMER 1993
  • Bajsiev Khadzhi-Murat Khasanovich
RU2046278C1
ELECTROPRIMER BUSH 1993
  • Bajsiev Khadzhi-Murat Khasanovich
RU2074385C1
ELECTRIC SQUIB 1992
  • Bajsiev Khadzhi-Murat Khasanovich
RU2046285C1
ROCKET SOLID FUEL ENGINE 1991
  • Bajsiev Khadzhi-Murat Khasanovich
RU2026501C1
METER FOR CLOUD CHARACTERISTICS 0
  • Bajsiev Khadzhi-Murat Khasanovich
SU1760483A1
SOLID ROCKET ENGINE 1989
  • Bajsiev Kh.-M.Kh.
RU1725598C
ANTI-HAIL ROCKET 2016
  • Bajsiev Khadzhi-Murat Khasanovich
RU2652595C2
DEVICE FOR DETERMINING STEAM-GAS MEDIUM PARAMETERS 0
  • Bajsiev Khadzhi-Murat Khasanovich
SU1765728A1
METAL OR METALLOID NANOPARTICLES PLASMAJET 2013
  • Starik Aleksandr Mikhajlovich
  • Kuleshov Pavel Sergeevich
  • Savel'Ev Aleksandr Mikhajlovich
RU2534762C1

RU 2 762 764 C1

Authors

Bajsiev Khadzhi-Murat Khasanovich

Nagoev Tamirlan Rustamovich

Dates

2021-12-22Published

2020-11-10Filed