Effect of Secondary Combustion on Thrust Regulation of Gas Generator Cycle Rocket Engine

Effect of Secondary Combustion on Thrust Regulation of Gas Generator Cycle Rocket Engine

Thrust regulation is applied to maintain the performance of the liquid propellant rocket engine. The thrust level of a rocket engine can be readily controlled by adjusting the number of propellants introduced into the combustion chamber. In this study, a gas generator design is proposed in which thr...

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Bibliographic Details
Main Authors: Sohaib Khan, Muhammad Umer Sohail, Ihtzaz Qamar, Muzna Tariq, Raees Fida Swati
Format: Article
Language:English
Published: MDPI AG 2022-10-01
Series:Applied Sciences
Subjects:
thrust regulation
secondary combustion
gas generator
liquid propellant rocket engine
chemical equilibrium
combustion modeling
Online Access:https://www.mdpi.com/2076-3417/12/20/10563

Internet

https://www.mdpi.com/2076-3417/12/20/10563

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