An experimental and modelling study of heat loads on a subscale methane rocket motor
Abstract
Given growing competition in the business space launch market, more researchers are evaluating the merit of methane as a potential propellant. In this study, a rocket combustion chamber with a single coaxial shear injector is tested. Gaseous oxygen and gaseous methane are employed in the hot firing tests at 2 MPa and a mass ratio of oxidizer to fuel of 2.65. Along the chamber axis, the wall temperatures are recorded; an inverse heat conduction...
Paper Details
Title
An experimental and modelling study of heat loads on a subscale methane rocket motor
Published Date
Nov 1, 2019
Journal
Volume
164
Pages
112 - 120
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