The Liquid Rocket Engine Design System Using a New Thermo-Gas-Dynamic Calculation Method

As is well known, the energy specifications of a liquid rocket engine (LRE) determine the structural scheme, optimal geometric, mass, thrust, flight specifications and the efficiency of the rocket. Therefore, in the calculation of the LRE energy characteristics special attention is paid to thermoche...

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Bibliographic Details

Published in:	Havacılık ve Uzay Teknolojileri Dergisi
Main Authors:	Parviz Shahmurad Abdullayev, Nijad Abdullah
Format:	Article
Language:	English
Published:	Turkish Air Force Academy 2019-07-01
Subjects:	Liquid Propellant Rocket Engine Combustion Chamber Nozzle Combustion Products Chemical Equilibrium Thermogasdynamic Calculation
Online Access:	http://www.jast.hho.edu.tr/JAST/index.php/JAST/article/view/378/300