END-TYPE IMPULSE PLASMA-JET ENGINE OPERATING ON SOLID PROPULSIVE MASS Russian patent published in 2000 - IPC

Abstract RU 2146776 C1

FIELD: electric jet engines. SUBSTANCE: device consists of central electrode - anode, cathode and solid propulsive grain placed in between. Anode has mechanical contact with solid mass, and cathode is arranged at a distance from solid grain to form vacuum space. Reactive thrust is formed by generating plasma by break-down and surface overlapping of solid mass by impulse of high tension energy of nanosecond duration of 10-9-10-6 from side of anode. EFFECT: simplified design, enhanced economy. 2 cl, 1 dwg

Similar patents RU2146776C1

Title Year Author Number
METHOD OF OBTAINING JET THRUST 1996
  • Vershinin Ju.N.
  • Nekrasov B.A.
RU2119594C1
PULSE ELECTRIC JET ENGINE 2001
  • Kazankin F.A.
  • Potabachnyj L.A.
  • Vershinin Ju.N.
  • Emlin R.V.
RU2211952C2
IMPULSE PLASMA ELECTRIC JET ENGINE 2002
  • Kazankin F.A.
  • Potabachnyj L.A.
  • Bukhvastov S.N.
RU2266428C2
IMPULSE PLASMA ELECTRIC JET ENGINE 2005
  • Potabachnyj Leonid Alekseevich
RU2319039C2
IMPULSE PLASMA ELECTRIC JET ENGINE 2007
  • Potabachnyj Leonid Alekseevich
  • Kazankin Filipp Andreevich
RU2358153C2
PROPULSION SYSTEM WITH PULSE ELECTRIC PROPULSION ENGINE 2016
  • Potabachnyj Leonid Alekseevich
RU2666918C2
PULSE ELECTRIC JET ENGINE 2011
  • Kazankin Filipp Andreevich
  • Potabachnyj Leonid Alekseevich
  • Ermilov Vitalij Anatol'Evich
RU2503848C2
METHOD OF DETERMINATION OF CURRENT WHICH FORMS HIGH-VOLTAGE BREAKDOWN CHANNEL IN CRYSTAL DIELECTRICS BY MEANS OF DEPENDENCE OF BREAKDOWN CHANNEL FORMATION SPEED FROM VOLTAGE 1996
  • Emlin R.V.
RU2108592C1
PULSED PLASMA ELECTRIC JET ENGINE 2017
  • Potabachnyj Leonid Alekseevich
RU2720602C2
CERMET CATHODE 1999
  • Kotov Ju.A.
  • Sokovnin S.Ju.
  • Balezin M.E.
RU2158982C1

RU 2 146 776 C1

Authors

Vershinin Ju.N.

Emlin R.V.

Il'Ichev D.S.

Potabachnyj L.A.

Kirillov S.A.

Kazankin F.A.

Dates

2000-03-20Published

1998-05-14Filed