RPA is a multi-platform analysis tool for conceptual and preliminary design of chemical rocket engines capable of: engine performance analysis, thrust chamber sizing, nozzle wall contour optimization, thrust chamber cooling analysis, engine cycle power balance analysis, engine mass estimation, scripting utility for development of custom solutions.

RPA is a multi-platform analysis tool for conceptual and preliminary design of chemical rocket engines capable of: engine performance analysis, thrust chamber sizing, nozzle wall contour optimization, thrust chamber cooling analysis, engine cycle power balance analysis, engine mass estimation, scripting utility for development of custom solutions.