Thermodynamically Modeled Non-equilibrium Structure of Combustion Products and Decomposition of Hydrazine-based Liquid Propellants
<p>The paper studies the emerging hallmarks and the characteristics of a two-parameter chemical non-equilibrium structure of the combustion products of liquid propellants as applied to the low-thrust liquid propellant engines (LT LPE) operating in the aircraft control system. The study is base...
| Main Authors: | , |
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| Format: | Article |
| Language: | Russian |
| Published: |
MGTU im. N.È. Baumana
2016-01-01
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| Series: | Nauka i Obrazovanie |
| Subjects: | |
| Online Access: | http://technomag.edu.ru/jour/article/view/859 |