Paper Title
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.