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


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Аннотация

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.

Авторлар туралы

E. Onufrieva

Bauman Moscow State Technical University

Email: Onufryev@bmstu.ru
Ресей, Moscow, 105005

V. Onufriev

Bauman Moscow State Technical University

Хат алмасуға жауапты Автор.
Email: Onufryev@bmstu.ru
Ресей, Moscow, 105005

Yu. Grishin

Bauman Moscow State Technical University

Email: Onufryev@bmstu.ru
Ресей, Moscow, 105005

N. Sidnyaev

Bauman Moscow State Technical University

Email: Onufryev@bmstu.ru
Ресей, Moscow, 105005

V. Sinyavsky

Korolev Rocket and Space Corporation Energia (RSC Energia)

Email: Onufryev@bmstu.ru
Ресей, Korolev, 141070

A. Ivashkin

Bauman Moscow State Technical University

Email: Onufryev@bmstu.ru
Ресей, Moscow, 105005

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