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Mission Profiles for the SUSAN Electrofan ConceptThe SUbsonic Single Aft eNgine (SUSAN) Electrofan is a novel aircraft concept which utilizes a single aft-mounted engine, electrified aircraft propulsion, an emergency backup battery, as well as state-of-the-art aerodynamic design and thermal management systems to reduce the overall environmental impact of the aircraft. Mission profiles, which define the aircraft state and flight characteristics throughout various phases of flight, are an important component of aircraft conceptual design. These defined characteristics can serve as sizing cases or design constraints. By defining the mission profiles to be within airworthiness certification standards and regulations, aircraft designers can ensure the conceptual design is predicted to be within compliance of these regulations throughout the design process. This paper will present mission profiles for the SUSAN Electrofan aircraft, including the basis for defining the characteristics required during each phase of flight.
Document ID
20220018208
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Casey L. Denham
(Langley Research Center Hampton, Virginia, United States)
Timothy Chau
(Science and Technology Corporation (United States) Hampton, Virginia, United States)
Wes Ryan
(Ames Research Center Mountain View, California, United States)
Ralph H. Jansen
(Glenn Research Center Cleveland, Ohio, United States)
Date Acquired
December 1, 2022
Subject Category
Aeronautics (General)
Meeting Information
Meeting: AIAA SciTech 2023
Location: National Harbor, MD
Country: US
Start Date: January 23, 2023
End Date: January 27, 2023
Sponsors: American Institute of Aeronautics and Astronautics
Funding Number(s)
WBS: 533127.02.22.07.05
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
Single Expert
Keywords
Conceptual Design
SUSAN Electrofan
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