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

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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.

Author(s): Ponomarenko A.

Language: English
Commentary: 1460760
Tags: Транспорт;Аэрокосмическая техника;Ракетные двигатели и энергетические установки