Pulsed plasma accelerator and method

Electric lamp and discharge devices: systems – Discharge device load with fluent material supply to the... – Plasma generating

Reexamination Certificate

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C315S111410, C315S111610

Reexamination Certificate

active

07408303

ABSTRACT:
A pulsed plasma accelerator includes two electrodes (1) arranged between dielectric bars (2) made from an ablating material, a discharge channel with an open end part whose walls are defined by the surfaces of electrodes (1) and dielectric bars (2), an energy accumulator (11) and current supplies (14,15) for connecting the electrodes (1) with the energy accumulator (11). The current supplies (14, 15) define in conjunction with the electrodes (1) and the energy accumulator (11) an external electric circuit, with characteristics of the external electric circuit being selected on the condition: 2≦C/L, where C (μF) is the electric capacitance of the external electric circuit, and L is the inductance of the external electric circuit, L≦100 nH. During operation of the plasma accelerator, quazi-nonperiodic pulse discharges are ignited and maintained in the discharge channel. By providing coordinated parameters of the external and internal circuits, a substantial increase in the efficiency of plasma acceleration is achieved.

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patent: 6200102 (2001-03-01), Diaz
patent: 6295804 (2001-10-01), Burton et al.
patent: 7183716 (2007-02-01), Kanarov et al.
patent: 2003/0033797 (2003-02-01), Spanjers et al.
patent: 2 143 586 (1999-12-01), None
Antropov, N, et al., “High efficiency ablative pulsed plasma thruster characteristics”,Proc. 3rdInternational Conference on Spacecraft Propulsion Cannes. Oct. 10-13, 2000,ESAP SP 465, Dec. 2002, 509-516.
Ziemer, J., et al., “Scaling laws for electromagnetic pulsed plasma thrusters”,Institute of Physics Publishing: Plasma Sources Sci., Technol., 10 (2001) 395-405.

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