FIELD: engines and pumps.
SUBSTANCE: invention relates to the engines on the Hall effect and particularly to the engine (1), downstream edge in the annular channel (2) thereof has a variable cross-section to allow change in thrust and specific impulse.
EFFECT: invention is aimed at producing an engine on the Hall effect capable of operating both in a high thrust mode and in a high specific impulse mode.
7 cl, 4 dwg
Title | Year | Author | Number |
---|---|---|---|
ENGINE FOR SPACECRAFT AND SPACECRAFT COMPRISING SUCH ENGINE | 2015 |
|
RU2678240C2 |
ENGINE ON THE HALL EFFECT | 2012 |
|
RU2620880C2 |
PLASMA JET ENGINE BASED ON HALL EFFECT | 2010 |
|
RU2555780C2 |
PLASMA ENGINE AND METHOD OF GENERATING ACTUATING PLASMA TRACTION | 2012 |
|
RU2610162C2 |
HALL-EFFECT ENGINE WITH CONTROLLED TEMPERATURE OF CATHODE HEATER | 2011 |
|
RU2564733C2 |
RAMJET RELATIVISTIC ENGINE | 2020 |
|
RU2776324C1 |
IONIC ROCKET ENGINE OF SPACECRAFT | 2018 |
|
RU2682962C1 |
SHORT-LENGTH PLASMA-JET ENGINE WITH CLOSED-CIRCUIT ELECTRON DRIFT | 1993 |
|
RU2107837C1 |
PLASMA JET ENGINE BASED ON HALL EFFECT | 2010 |
|
RU2527267C2 |
ROCKET LABORATORY ENGINE BASED ON HALL EFFECT AND TEST BENCH | 2020 |
|
RU2740078C1 |
Authors
Dates
2017-05-15—Published
2013-02-05—Filed