Whether your focus is phase-A propulsion engineering, vehicle design, or technology prioritization, the ability to quickly predict liquid rocket engine performance can be critical. With REDTOP-Lite, you can obtain realistic engine thrust, specific impulse, weight, and nozzle geometry information based on just a handful of top-level engine design input parameters.
REDTOP-Lite analyzes the main chamber and nozzle components of a liquid rocket engine to determine the engine's operating performance and geometric parameters. The engine may be sized based on one of several approaches, including matching a specified thrust level, throat area, exit area, or total propellant flowrate. REDTOP-Lite really is “built for design”.
REDTOP-Lite's chemistry model utilizes a robust and industry-accepted technique based on minimizing the Gibbs Free Energy to obtain equilibrium combustion products quickly and with appropriate accuracy. The design of the equilibrium model makes it easy for you to add new fuels, oxidizers, and combustion products.
REDTOP-Lite offers several features that separate it from the competition and make it even easier for you to get the job done right.
REDTOP-Lite software is sold with a perpetual license to use the particular version that is purchased. The perpetual license does not require an annual maintenance fee for continued use. Minor bug fixes may be released to all license-holders from time to time free of charge. License-holders may choose to purchase new and updated versions of our software as they are released.
Windows |
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| Operating System Requirements | Windows 7, Vista, or XP |
| Additional Notes | Run from a windows GUI or via command line |
| Microsoft Excel-based interface option is also available for running the tool | |