Preliminary Design and Simulation of a Thermal Management System with Integrated Secondary Power Generation Capability for a Mach 8 Aircraft Concept Exploiting Liquid Hydrogen

Preliminary Design and Simulation of a Thermal Management System with Integrated Secondary Power Generation Capability for a Mach 8 Aircraft Concept Exploiting Liquid Hydrogen

This paper introduces the concept of a thermal management system (TMS) with integrated on-board power generation capabilities for a Mach 8 hypersonic aircraft powered by liquid hydrogen (LH2). This work, developed within the EU-funded STRATOFLY Project, aims to demonstrate an opportunity for facing...

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Bibliographic Details
Main Authors: Davide Ferretto, Nicole Viola
Format: Article
Language:English
Published: MDPI AG 2023-02-01
Series:Aerospace
Subjects:
thermal management system
on-board power generation
hypersonic aircraft
regenerative cooling
liquid hydrogen
on-board system simulation
Online Access:https://www.mdpi.com/2226-4310/10/2/180

Internet

https://www.mdpi.com/2226-4310/10/2/180

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