The Thermal State Computational Research of the Low-Thrust Oxygen-Methane Gaseous-Propellant Rocket Engine in the Pulse Mode of Operation

The Thermal State Computational Research of the Low-Thrust Oxygen-Methane Gaseous-Propellant Rocket Engine in the Pulse Mode of Operation

<p>Currently promising development direction of space propulsion engineering is to use, as spacecraft controls, low-thrust rocket engines (RDTM) on clean fuels, such as oxygen-methane. Modern RDTM are characterized by a lack regenerative cooling and pulse mode of operation, during which there...

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Bibliographic Details
Main Authors: O. A. Vorozheeva, D. A. Yagodnikov
Format: Article
Language:Russian
Published: MGTU im. N.È. Baumana 2014-01-01
Series:Nauka i Obrazovanie
Subjects:
low-thrust rocket engine
gaseous oxygen
gaseous methane
pulse mode
thermal state
Online Access:http://technomag.edu.ru/jour/article/view/740

Internet

http://technomag.edu.ru/jour/article/view/740

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