METHOD OF AND DEVICE FOR REGULATION OF THRUST OF ELECTRIC ROCKET PLASMA ENGINE

FIELD: electric rocket engines. SUBSTANCE: according to proposed method, thrust of electric rocket plasma engine is regulated by changing rate of working medium so that value of engine thrust proportional to product should remain maximum possible where Ia is current flowing through anode and Ua is v...

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Bibliographic Details
Main Authors VOLKOV M.P, GORDEEV K.G, GOROSHKOV I.N, GALAJKO V.N, SHINJAKOV JU.A
Format Patent
LanguageEnglish
Russian
Published 20.06.2003
Edition7
Subjects
BLASTING
HEATING
LIGHTING
MACHINES OR ENGINES FOR LIQUIDS
MECHANICAL ENGINEERING
OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
PRODUCING A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDEDFOR
PRODUCING MECHANICAL POWER
WEAPONS
WIND, SPRING WEIGHT AND MISCELLANEOUS MOTORS
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Summary:FIELD: electric rocket engines. SUBSTANCE: according to proposed method, thrust of electric rocket plasma engine is regulated by changing rate of working medium so that value of engine thrust proportional to product should remain maximum possible where Ia is current flowing through anode and Ua is value of anode voltage. For this purpose extreme regulator is introduced additionally into known thrust stabilizer. EFFECT: improved efficiency of electric rocket plasma engine operating as cruise engine. 3 cl, 3 dwg
Bibliography:Application Number: RU20010117800