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Center for High-Efficiency Electrical Technologies for Aircraft: Phase I Final ReportUnder the University Leadership Initiative (ULI), the Center for High-Efficiency for Electrical Technologies (CHEETA) was established to develop and mature early-stage technologies pertaining to hydrogen-electric power and energy systems for aircraft. In particular, integration of these technologies on an aircraft system is envisioned to leverage the high specific energy content of liquid hydrogen (LH2) with fuel cell energy conversion and an electrically driven ducted fan system to provide an ultra-efficient propulsion drivetrain. For this concept, the LH2 system is not just used as an energy storage mechanism, but also as a cryogen to enable highly efficient superconducting electric systems. The end result of this concept is an integrated aircraft system with a quiet, efficient propulsion architecture that produces zero CO2, NOx, SOx, and particulate matter emissions at the vehicle level.
Document ID
20260001562
Acquisition Source
Glenn Research Center
Document Type
Contractor Report (CR)
Authors
Phillip J Ansell
(University of Illinois Urbana-Champaign Urbana, United States)
Kiruba Haran
(University of Illinois Urbana-Champaign Urbana, United States)
Michael Sumption
(The Ohio State University Columbus, United States)
Wolfgang Stautner
(General Electric (United States) Boston, United States)
David Hall
(Pennsylvania State University State College, United States)
Alan Mantooth
(University of Arkansas at Fayetteville Fayetteville, United States)
Edward Greitzer
(Massachusetts Institute of Technology Cambridge, United States)
Fang Luo
(Stony Brook University Stony Brook, United States)
Kai James
(University of Illinois Urbana-Champaign Urbana, United States)
Jason Merret
(University of Illinois Urbana-Champaign Urbana, United States)
Timothy Haugan
(United States Air Force Research Laboratory Wright-Patterson AFB, United States)
Luigi Vanfretti
(Rensselaer Polytechnic Institute Troy, United States)
Mary Ann Sebastian
(University of Dayton Research Institute)
Michael Stoia
(Boeing Research and Technology Huntington Beach, California)
Date Acquired
February 19, 2026
Publication Date
May 1, 2026
Publication Information
Publisher: National Aeronautics and Space Administration
Subject Category
Aircraft Propulsion and Power
Report/Patent Number
NASA/CR-20260001562
E20333
Funding Number(s)
CONTRACT_GRANT: 80NSSC19M0125
Distribution Limits
Public
Copyright
Use by or on behalf of the US Gov. Permitted.
Technical Review
NASA Technical Management
Keywords
Hydrogen
Boundary Layer Ingestion
Distributed Propulsion
Superconducting Electric Machine
Superconducting Power Transfer
Fuel Cell
Cryogenic Electrical Systems
Aerodynamics
Aircraft Propulsion
High-Lift
MDAO
Hydrogen Tank
Two-phase Flow
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