On Calculation of the Ignition Voltage for a Back-Arc Discharge in a High-Voltage Thermionic Diode


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详细

Development of large spacecraft propulsion units involves the creation of high-temperature radiation-resistant systems for current conversion based on thermionic devices of plasma electric power engineering, such as grid-controlled switches and high-voltage plasma thermionic diodes (HVPTD). The current conversion system (CCS) is required to match the electrical parameters of a thermionic conversion power reactor (with an output voltage of 120–150 V) with the parameters of the electric jet engine (having a working voltage of hundreds or thousands of volts). This brings about an urgent issue of calculating the ignition voltage for the back-arc discharge in the interelectrode gap (IEG) of HVPTDs. A semiempirical correlation is proposed for predicting the back-arc discharge ignition voltage as a function of the cesium vapor pressure in IEG and the anode temperature. It can be used by designers of thermionic plasma power engineering devices.

作者简介

E. Onufrieva

Bauman Moscow State Technical University

Email: Onufryev@bmstu.ru
俄罗斯联邦, Moscow, 105005

V. Onufriev

Bauman Moscow State Technical University

编辑信件的主要联系方式.
Email: Onufryev@bmstu.ru
俄罗斯联邦, Moscow, 105005

Yu. Grishin

Bauman Moscow State Technical University

Email: Onufryev@bmstu.ru
俄罗斯联邦, Moscow, 105005

N. Sidnyaev

Bauman Moscow State Technical University

Email: Onufryev@bmstu.ru
俄罗斯联邦, Moscow, 105005

V. Sinyavsky

Korolev Rocket and Space Corporation Energia (RSC Energia)

Email: Onufryev@bmstu.ru
俄罗斯联邦, Korolev, 141070

A. Ivashkin

Bauman Moscow State Technical University

Email: Onufryev@bmstu.ru
俄罗斯联邦, Moscow, 105005

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