FIELD: engines and pumps.
SUBSTANCE: proposed anode comprises case, input and output commutators. Note here that input commutator is connected with isolated anode lines and has perforations to communicate it with output commutator provided with system of holes. Note also that input commutator is made up of two air-isolated commutators tightly connected with appropriate isolated anode lines. Mind that every input commutator incorporates holes to it to be communicated with output commutator.
EFFECT: reduced weight of propulsion unit, higher reliability and longer life.
Title | Year | Author | Number |
---|---|---|---|
METHOD FOR DEFINITION OF FLOW RATE OF SYSTEM FOR SUPPLY OF WORKING MEDIUM TO PLASMA SOURCE | 2008 |
|
RU2392589C2 |
METHOD FOR TIGHTNESS DETECTION OF SYSTEM FOR WORKING FLUID SUPPLY TO SOURCE OF PLASMA, PREFERABLY UNDER VACUUM CONDITIONS | 2008 |
|
RU2377522C1 |
SIMULATOR OF ELECTRIC ROCKET PLASMA PROPULSION PLANT | 2009 |
|
RU2395716C1 |
DYNAMIC SIMULATOR OF STATIONARY PLASMA ENGINES | 2015 |
|
RU2610623C1 |
ENGINE WITH CLOSED DRIFT OF ELECTRONS | 2012 |
|
RU2524315C2 |
METHOD OF LAUNCH AND POWER SUPPLY OF ELECTROJET PLASMA ENGINE (VERSIONS) AND DEVICE FOR ITS IMPLEMENTATION (VERSIONS) | 2008 |
|
RU2366123C1 |
METHOD FOR CONTROLLING A STATIONARY PLASMA ENGINE | 2016 |
|
RU2647749C2 |
ELECTRIC ROCKET ENGINE (VERSIONS) AND METHOD OF OPERATION OF SUCH ENGINE | 2005 |
|
RU2309293C2 |
PLASMA ENGINE WITH CLOSED DRIFT OF ELECTRONS | 2010 |
|
RU2426007C1 |
DEVICE FOR GROUND TESTING OF PNEUMATIC SYSTEM OF ELECTRIC ROCKET ENGINE INSTALLATION | 1994 |
|
RU2097601C1 |
Authors
Dates
2011-06-20—Published
2008-09-18—Filed