RPA: Tool for Rocket Propulsion Analysis. Thermal Analysis of Thrust Chambers

2012, 26 с. RPA (Rocket Propulsion Analysis) is a multi-platform analysis tool intended for use in conceptual and preliminary design of rocket engines. This article describes a numerical model of thermal analysis of cooled combustion chambers and nozzles, implemented as a Thermal Analysis Module for RPA. From the component design, to the subsystem design, to the engine systems design, engine development and flight-vehicle application, this how-to text bridges the gap between basic physical and design principles and actual rocket-engine design as it's done in industry.