FIELD: engines.
SUBSTANCE: invention relates to electric rocket propulsion systems with electromagnetic acceleration of plasma. Electric propulsion system comprises power plant, system for storage and supply of working medium and electric jet engine. Device comprises coaxially mounted cathode, nozzle-anode and solenoid arranged outside nozzle-anode. Power plant and solenoid are connected through current leads with motor-generator. Flywheel and electric rocket engine are coaxially fixed at motor-generator shaft. Device is connected with system of storage and supply of working medium through insulating spacer and channel made inside shaft of electric motor-generator.
EFFECT: technical result is reduction of weight of power plant and higher thrust of electric rocket propulsion system.
1 cl, 1 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| NUCLEAR POWER PROPULSION UNIT | 2018 |
|
RU2676675C1 |
| ELECTRIC ROCKET ENGINE PLANT AND METHOD OF ITS OPERATION | 2005 |
|
RU2308610C2 |
| METHOD OF BRINGING TO A GIVEN INTERPLANETARY ORBIT AND A REUSABLE TRANSPORT-ENERGY MODULE | 2018 |
|
RU2728180C2 |
| SPACECRAFT NUCLEAR PROPULSION SYSTEM | 2013 |
|
RU2533672C1 |
| METHOD OF ORBITING SPACECRAFT FROM TRANSFER ORBIT TO GEOSTATIONARY ORBIT | 2009 |
|
RU2408506C1 |
| WAVE ION ENGINE WITH A CLOSED GAS DISCHARGE CHAMBER | 2021 |
|
RU2771908C1 |
| STAND FOR TESTING ELECTRIC ROCKET ENGINE OPERATING ON IODINE WORKING BODY AND METHOD FOR TESTING ELECTRIC ROCKET ENGINE OPERATING ON IODINE WORKING BODY | 2016 |
|
RU2641983C2 |
| MULTICHANNEL PLASMA ENGINE WITH A HEMISPHERICAL GAS-DISCHARGE CHAMBER | 2022 |
|
RU2796728C1 |
| IONIC ROCKET ENGINE OF SPACECRAFT | 2018 |
|
RU2682962C1 |
| ELECTRIC JET PROPULSION PLANT | 2018 |
|
RU2727103C2 |
