scorpaena : Data for Ethanol and Kerosene Propellant for Gas-Generator Fed Upper Stage Application

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This repository contains results of the cycle analysis of LOx/Ethanol liquid rocket engine based on the gas-generator cycle using EcoSimPro for steady-state operation [1]. Similar data on LOx/RP-1 with the same class and design requirements are given for performance evaluation. The relations of specific impulse to the oxidizer-to-fuel ratio and specific impulse to the exhaust pressure are constructed and can be used in design calculations.



Simplified transient model for LOx/Ethanol performance evaluation [1]



Source:

[1] Robson Henrique dos Santos Hahn, Jan Deeken, Stefan Schlechtriem. (2017). Comparative Study of Ethanol and Kerosene Propellant for Gas-Generator Fed Upper Stage Application, Using EcoSimPro. 31st International Symposium on Space Technology and Science, June 2017

This repository contains results of the cycle analysis of LOx/Ethanol liquid rocket engine based on the gas-generator cycle using EcoSimPro for steady-state operation [1]. Similar data on LOx/RP-1 with the same class and design requirements are given for performance evaluation. The relations of specific impulse to the oxidizer-to-fuel ratio and specific impulse to the exhaust pressure are constructed and can be used in design calculations.



Simplified transient model for LOx/Ethanol performance evaluation [1]



Source:

[1] Robson Henrique dos Santos Hahn, Jan Deeken, Stefan Schlechtriem. (2017). Comparative Study of Ethanol and Kerosene Propellant for Gas-Generator Fed Upper Stage Application, Using EcoSimPro. 31st International Symposium on Space Technology and Science, June 2017

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