超声速氩气在电弧推力器中的流动参数

PROGRESS IN DETONATION RESEARCH Pub Date : 2020-10-16 DOI:10.30826/icpcd12a29

V. Gorbunkov, V. V. Shalay, N. V. Pustovoi

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引用次数: 0

摘要

航天器轨道修正推进系统的一个特点是，气体等离子体占据一个小的封闭空间。在局部局部热平衡近似下，利用发射光谱法计算了PSSC腔内氩气的温度。

本文章由计算机程序翻译，如有差异，请以英文原文为准。

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THE SUPERSONIC ARGON FLOW PARAMETERS IN AN ARCJET THRUSTER

A small closed volume occupied by the gas plasma is a specific feature of the propulsion systems for orbit correction of spacecraft (PSSC). We found the temperature of argon in the PSSC chamber using emission spectroscopy methods in the approximation of partial local thermal equilibrium.

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PROGRESS IN DETONATION RESEARCH

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