NASA collaborates with U.S. industry to conduct conceptual design studies for various electrified aircraft configurations that could help improve fuel efficiency and vehicle performance. Covering a range of aircraft sizes, markets, and operating timeframes, these concepts help determine technological requirements for each configuration along with estimates for fuel savings and emission reductions.
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Types of Electrified Aircraft
NASA is exploring six different propulsion system architectures for future electrified aircraft, ranging from fully electric systems to hybrid and turboelectric configurations.
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Vehicle Designs
Explore NASA's fleet of electrified aircraft concepts and learn how each vehicle configuration offers unique performance benefits.

SUSAN Electrofan
The SUbsonic Single Aft eNgine (SUSAN) Electrofan is a hybrid electric aircraft concept designed for reducing fuel burn in future single-aisle commercial aircraft.

N3-X
The N3-X is a fully turboelectric aircraft concept designed with a hybrid wing body airframe to maximize aerodynamic efficiency and reduce energy usage.

STARC-ABL
The Single-Aisle Turboelectric Aircraft with Aft Boundary Layer Propulsion (STARC-ABL) is a partially turboelectric aircraft concept designed to optimize performance with improved aerodynamics.