METHOD OF AND DEVICE FOR REGULATION OF THRUST OF ELECTRIC ROCKET PLASMA ENGINE Russian patent published in 2003 - IPC

Abstract RU 2206787 C2

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 I_a is current flowing through anode and U_a 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

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RU 2 206 787 C2

Authors

Shinjakov Ju.A.

Galajko V.N.

Volkov M.P.

Gordeev K.G.

Goroshkov I.N.

Dates

2003-06-20—Published

2001-06-26—Filed