Introducing Rocket Propulsion Analysis Lite x64 - a cutting-edge software for designing rocket engines. Developed by Alexander Ponomarenko, this program delivers advanced analysis and simulation tools for the best possible rocket design. With its user-friendly interface and intuitive features, Rocket Propulsion Analysis Lite x64 is perfect for engineers and enthusiasts alike. Don't miss out on this powerful tool - download now!

Rocket Propulsion Analysis (RPA) is a multi-platform rocket engine analysis tool for rocketry professionals, scientists, students and amateurs.

For many years rocketry scientists, students and amateurs were using command-line MS-DOS or UNIX programs to calculate the performance of the rocket engines. While the accuracy of the old programs is still sufficient for many cases, the old-fashioned interface has poor usability, whereas the lack or absence of active development makes it difficult to satisfy new user requirements.

With release of the RPA Lite Edition, software.lpre.de offers the modern rocket engines analysis tool and promises continuous further development of the program.

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.

By providing a few engine parameters such as combustion chamber pressure, used propellant components, and nozzle parameters, the program obtains chemical equilibrium composition of combustion products, determines its thermodynamic properties, and predicts the theoretical rocket performance. The results of calculation can also be used to design combustion chambers, gas generators and preburners of the liquid propellant rocket engines.

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)
Multi-platform graphical user interface for Microsoft® Windows™ (both x86 and x86-64), as well as for Apple® Mac OS X and Linux
Embedded species database editor

Hyperlink code:
Hyperlink and Intro code:
Hyperlink for Forum code:

All Rocket Propulsion Analysis Lite x64 reviews, submitted ratings and written comments become the sole property of Windows 7 download. You acknowledge that you, not windows7download, are responsible for the contents of your submission. However, windows7download reserves the right to remove or refuse to post any submission for any reason.

Windows 7 Download periodically updates pricing and software information of Rocket Propulsion Analysis Lite x64 full version from the publisher, but some information may be out-of-date. You should confirm all information.
Using warez version, crack, warez passwords, patches, serial numbers, registration codes, key generator, pirate key, keymaker or keygen for Rocket Propulsion Analysis Lite x64 license key is illegal and prevent future development of Rocket Propulsion Analysis Lite x64. Download links are directly from our mirrors or publisher's website, Rocket Propulsion Analysis Lite x64 torrent or shared files from free file sharing and free upload services, including Rapidshare, MegaUpload, YouSendIt, SendSpace, DepositFiles, DivShare, HellShare, HotFile, FileServe or MediaFire, are not used.