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Francesco Barato

As seen in: MDPI
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Articles

Design and Analysis of a Micro-Electro-Mechanical System Thruster for Small Satellites and Low-Thrust Propulsion

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By Yubin Zhong, Fabrizio Ponti, Francesco Barato, Guojun Xia
| MDPI
All articles published by MDPI are made immediately available worldwide under an open access license. No special permission is required to reuse all or part of the article published by MDPI, including figures and tables. For articles published under an open access Creative Common CC BY license, any part of the article may be reused without permission provided that the original article is clearly cited. For more information, please refer to https://www.mdpi.com/openaccess.
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Review of Alternative Sustainable Fuels for Hybrid Rocket Propulsion

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By Francesco Barato
| MDPI
This is an early access version, the complete PDF, HTML, and XML versions will be available soon.
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A Simplified Thermal Analysis Model for Regeneratively Cooled Rocket Engine Thrust Chambers and Its Calibration with Experimental Data

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By Francesco Barato, Marco Pizzarelli, Matteo Fagherazzi, Marco Santi
| MDPI
Abstract : An essential part of the design of a liquid rocket engine is the thermal analysis of the thrust chamber, which is a component whose operative life is limited by the maximum allowable wall temperature and heat flux. A simplified steady-state thermal analysis model for regeneratively cooled rocket engine thrust chambers is presented.
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