FIELD: engines and pumps.
SUBSTANCE: invention relates to space engineering and can be used to accelerate space crafts in deep vacuum conditions. The proposed engine represents a three-section axially symmetric metal chamber arranged, partially, inside a magnetic coil with the said sections being electrically isolated from each other. The first section, if seen from left to right, accommodates the gas discharge igniter with a circular hollow cathode, the second section housing an axial-side tubular intermediate anode. The third section houses the main anode representing an elongated cylinder with its right head face closed by electrically isolated output electrode with an axial-side orifice for plasma efflux. The said main anode is fitted inside the solenoid, the output electrode comprising a correction solenoid and making a part of the three-electrode acceleration system.
EFFECT: possibility to apply high potential differences approximating to 10 to 100 kV without breakdown between acceleration system electrodes.
Title | Year | Author | Number |
---|---|---|---|
HIGH-VOLTAGE ION ENGINE FOR SPACE VEHICLES | 2008 |
|
RU2411393C2 |
ION SOURCE | 0 |
|
SU818366A1 |
DEVICE FOR CREATION OF ADJUSTABLE THRUST FORCE IN ELECTRIC ION ENGINE | 2018 |
|
RU2704523C1 |
IONIC ROCKET ENGINE OF SPACECRAFT | 2018 |
|
RU2682962C1 |
RAMJET RELATIVISTIC ENGINE | 2020 |
|
RU2776324C1 |
PLASMA ACCELERATOR DEVICE | 2002 |
|
RU2275761C2 |
DEVICE FOR INCREASING THRUST IN AN ELECTRIC ION THRUSTER | 2022 |
|
RU2784248C1 |
IONIC ENGINE | 2014 |
|
RU2565646C1 |
HIGH-FREQUENCY PLASMA SOURCE | 2022 |
|
RU2789534C1 |
ION SOURCE | 2020 |
|
RU2749668C1 |
Authors
Dates
2009-02-27—Published
2007-10-24—Filed