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Parametric Modeling and Mission Optimization for the Hybrid Electric Turboprop Commercial Freighter (HETCOF) ConceptThe Hybrid Electric Turboprop Commercial Freighter (HETCOF) Concept is a large, four-engine turboprop freighter retrofitted with a multi-Megawatt parallel-hybrid electric propulsion system that aims to reduce emissions, noise, and fuel consumption for narrowbody cargo operations. This paper provides a detailed overview of the parametric modeling of HETCOF configurations across varying technology levels and optimization of the power-split profiles and mission trajectories for both the long range 2,400 NM economic mission and 750 NM hybrid-electric design mission. Results demonstrate that the HETCOF concept can achieve 11-13% fuel savings for the maximum range 2,400 NM mission with up to 38% fuel savings for the hybrid-electric 750 NM mission assuming all-electric cruise. Trade-offs in payload capacity are driven by weight of electric power and energy storage systems which can be minimized through coupled motor-propeller optimization and refined engine controls throughout the multi-phase design mission. Preliminary results demonstrate that HETCOF can realize meaningful operational benefits that scale with improved technology levels, where future work will aim to quantify the fleet-level impacts.
Document ID
20250004950
Acquisition Source
Ames Research Center
Document Type
Extended Abstract
Authors
Dahlia D. V. Pham
(Ames Research Center Mountain View, United States)
Carlos Anthony D. Natividad
(Ames Research Center Mountain View, United States)
Benjamin W. L. Margolis
(Ames Research Center Mountain View, United States)
Noah S. Listgarten
(Ames Research Center Mountain View, United States)
Ralph H. Jansen
(Glenn Research Center Cleveland, United States)
Date Acquired
May 12, 2025
Subject Category
Aircraft Design, Testing and Performance
Aircraft Propulsion and Power
Aeronautics (General)
Meeting Information
Meeting: AIAA SciTech Forum
Location: Orlando, FL
Country: US
Start Date: January 12, 2026
End Date: January 16, 2026
Sponsors: American Institute of Aeronautics and Astronautics
Funding Number(s)
PROJECT: 770848
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Technical Review
NASA Peer Committee
Keywords
hybrid-electric aircraft
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