SPACE VEHICLE ELECTRICATION REGULATOR Russian patent published in 2022 - IPC B64G1/52 H05F3/00 

Abstract RU 2771059 C1

FIELD: electrical engineering.

SUBSTANCE: invention relates to the field of electrical engineering, in particular to the field of space technology, and can be used to eliminate the accumulated static surface charges (electrons) on the elements of the outer structure of spacecraft. The electrification regulator (ER) of the spacecraft contains sensors for controlling the level of electrification of the spacecraft surface fragments and plasma engines with systems for power supply, control and supply of the working fluid to the engine chambers. Spacecraft ER also contains accelerator channels (AC) of plasma engines, which in the zone of low-temperature plasma creation are connected by side inlet gas lines, which have semi-cylindrical intake shells at the beginning in the AC, and side outlet gas lines with electrovalves located on them with neutralizers limited from all sides and communicating with the external environment through only gas lines. The composition of the gas mains includes metallized fragments of the spacecraft surface and thermoelements rigidly placed on them and having a galvanic connection with them.

EFFECT: emission of electrons of differential charging from the surfaces of the spacecraft that are in contact with the PD plasma is improved.

1 cl, 2 dwg

Similar patents RU2771059C1

Title Year Author Number
METHOD OF SPACECRAFT ELECTRIZATION CONTROL AND DEVICE FOR ITS ACCOMPLISHMENT 1990
  • Вabkin G.V.
  • Juldashev Еh.М.
RU2020776C1
METHOD OF FORMATION OF ELECTRIC PULSES SIMULATING ELECTROSTATIC DISCHARGES FROM SPACECRAFT PLASMA ENGINE ELEMENTS AND DEVICE FOR ITS IMPLEMENTATION 2014
  • Katasonov Nikolaj Mikhajlovich
RU2566809C1
CYCLOTRON PLASMA ENGINE 2012
  • Afanas'Ev Sergej Mikhajlovich
RU2517004C2
CYCLOTRON PLASMA ENGINE 2014
  • Afanasev Sergej Mikhajlovich
RU2578551C2
METHOD OF LAUNCH AND POWER SUPPLY OF ELECTROJET PLASMA ENGINE (VERSIONS) AND DEVICE FOR ITS IMPLEMENTATION (VERSIONS) 2008
  • Kozubskij Konstantin Nikolaevich
  • Murashko Vjacheslav Mikhajlovich
  • Gopanchuk Vladimir Vasil'Evich
  • Olotin Sergej Vladimirovich
RU2366123C1
SYSTEM FEED WORKING MEDIUM OF PLASMA ACCELERATORS (VERSIONS) 1992
  • Korolev S.K.
  • Kozubskij K.N.
  • Komarov G.A.
  • Kondakov Ju.G.
RU2032282C1
RAMJET RELATIVISTIC ENGINE 2020
  • Senkevich Aleksandr Pavlovich
RU2776324C1
IONIC ROCKET ENGINE OF SPACECRAFT 2018
  • Tsybin Oleg Yurevich
  • Makarov Sergej Borisovich
RU2682962C1
METHOD OF FORMING DUST FLOW FOR SPACECRAFT INTERORBITAL MANEUVER AND SYSTEM FOR ITS IMPLEMENTATION 2023
  • Razumnyi Iurii Nikolaevich
  • Kupreev Sergei Alekseevich
  • Razumnyi Vladimir Iurevich
  • Samusenko Oleg Evgenevich
RU2821855C1
POWER SUPPLY AND CONTROL METHOD FOR SPACECRAFT CORRECTION SYSTEM 2013
  • Testoedov Nikolaj Alekseevich
  • Jakimov Evgenij Nikolaevich
  • Sedykh Oleg Jur'Evich
  • Grafodatskij Oleg Sergeevich
  • Sevast'Janov Nikolaj Nikolaevich
  • Kundik Viktor Aleksandrovich
  • Murashko Vjacheslav Mikhajlovich
  • Lesnevskij Vladimir Aleksandrovich
  • Gordeev Konstantin Grigor'Evich
  • Galajko Vladimir Nikolaevich
  • Ostapushchenko Aleksandr Anatol'Evich
  • Gladushchenko Vladimir Nikolaevich
RU2549318C2

RU 2 771 059 C1

Authors

Afanasev Sergei Mikhailovich

Dates

2022-04-25Published

2021-11-10Filed