FIELD: engines and pumps.
SUBSTANCE: invention relates to electric rocket engines. Proposed engine comprises electromagnet, magnetic core with poles, anode and neutralizer cathode rigidly coupled with magnetic core and circular discharge chamber secured at the flange spring-loaded relative to magnetic core, while flange with circular discharge chamber secured thereat is coupled with the rod. Opposite end of said rod is connected with magnetic core. Note here that said rod is made of material with creep rate equal to linear rate of discharge chamber wall erosion.
EFFECT: continuous recovery of discharge chamber geometry, longer life, keeping high operating performances.
3 dwg
Title | Year | Author | Number |
---|---|---|---|
COMPOUND ENGINE WITH ANODE LAYER (VERSIONS) | 2008 |
|
RU2406873C2 |
PLASMA ACCELERATOR WITH CLOSED ELECTRON DRIFT | 2010 |
|
RU2447625C2 |
ENGINE WITH CLOSED DRIFT OF ELECTRONS | 2012 |
|
RU2524315C2 |
PLASMA ENGINE WITH CLOSED ELECTRON DRIFT | 2017 |
|
RU2668588C2 |
PLASMA ENGINE WITH CLOSED ELECTRINE DRIFT | 2008 |
|
RU2371605C1 |
CLOSED-ELECTRON-DRIFT PLASMA ACCELERATOR | 1998 |
|
RU2139646C1 |
PLASMA ACCELERATOR WITH CLOSED ELECTRON DRIFT | 2001 |
|
RU2209533C2 |
IONIC ENGINE | 2014 |
|
RU2565646C1 |
PLASMA ENGINE WITH CLOSED ELECTRON DRIFT | 2008 |
|
RU2377441C1 |
PLASMA ACCELERATOR WITH CLOSED ELECTRON DRIFT | 2017 |
|
RU2659009C1 |
Authors
Dates
2015-06-27—Published
2013-09-11—Filed