Rocket Propulsion Analysis Lite A complex tool for rocket propulsion analysis.
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Rocket Propulsion Analysis Lite Description

RPA is an easy-to-use multi-platform tool for the performance prediction of rocket engines. It features an intuitive graphical user interface with convenient grouping the input parameters and analysis results. RPA utilizes an expandable chemical species library based on NASA Glenn thermodynamic database and Gurvich thermodynamic database, that includes data for numerous fuels and oxidizers, such as liquid hydrogen and oxygen, kerosene, hydrogen peroxide, MMH, and many others. With embedded species editor, the users may also easily define new propellant components, or import components from PROPEP or CEA2 species databases. Give Rocket Propulsion Analysis Lite a try to fully assess its capabilities! Main features: Robust, proven and industry-accepted Gibbs free energy minimization approach is used to obtain the combustion composition Analysis of nozzle flows with shifting and frozen chemical equilibrium Optimisation of propellant components mixture ratio for maximum specific impulse of bipropellant systems Altitude performance analysis Analysis of nozzle performance with respect to overexpansion and flow separation Throttled engine performance analysis Estimation of test (actual) nozzle performance Nested analysis, stepping of up to four independent variables (component ratio, chamber pressure, nozzle inlet conditions, nozzle exit conditions) Embedded species database editor

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