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Thermal Management System Trade Study for SUSAN Electrofan AircraftThermal management of power system components is one of the barriers identified towards the implementation of Electrified Aircraft Propulsion architectures. This paper documents the preliminary results of a trade space exploration of thermal management systems conducted for a new National Aeronautics and Space Administration regional transport aircraft concept called the SUbsonic Single Aft eNgine (SUSAN) Electrofan. Traditional methods of thermal management are evaluated alongside newer methods, which are still in development. Mass, power, and drag for traditional liquid / air heat exchangers were calculated, along with mass and area of oscillating heat pipes for outer mold line cooling. An initial assessment of the feasibility of using the fuel as part of the thermal management system was also conducted by evaluating the temperature over the full flight profile. Preliminary results and future work are discussed.
Document ID
20210024094
Document Type
Conference Paper
Authors
Nic Heersema (Armstrong Flight Research Center Rosamond, California, United States)
Ralph H Jansen (Glenn Research Center Cleveland, Ohio, United States)
Date Acquired
November 8, 2021
Subject Category
Fluid Mechanics and Thermodynamics
Meeting Information
AIAA SciTech Forum(San Diego, CA)
Funding Number(s)
WBS: 981698
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Technical Review
NASA Peer Committee

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NameType 20210024094 FINAL.pdf STI