Analytical Investigation of Propellant Flow of Wall Structure For a Bi-Propellant Thruster
In this paper, a bi – propellant thruster will be designed by varying parameters ambient pressure, chamber
pressure, desired thrust using theoretical calculations. 3D models of the thruster will be done in Pro/Engineer. CFD analysis
will be done to determine the pressure, heat transfer coefficients, heat transfer rates and mass flow rates. Structural analysis
will be done by applying the pressures obtained from CFD analysis to determine stresses and displacements. Thermal
analysis will also be performed to determine heat transfer rates. Analysis will be done in Ansys.