NDLI: Turboelectric aircraft drive key performance parameters and functional requirements (Document No: 20150016906)

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Turboelectric aircraft drive key performance parameters and functional requirements (Document No: 20150016906)

Content Provider	NASA Technical Reports Server (NTRS)
Author	Felder, James L. Duffy, Kirsten P. Jansen, Ralph H. Brown, Gerald V.
Copyright Year	2015
Description	The purpose of this paper is to propose specific power and efficiency as the key performance parameters for a turboelectric aircraft power system and investigate their impact on the overall aircraft. Key functional requirements are identified that impact the power system design. Breguet range equations for a base aircraft and a turboelectric aircraft are found. The benefits and costs that may result from the turboelectric system are enumerated. A break-even analysis is conducted to find the minimum allowable electric drive specific power and efficiency that can preserve the range, initial weight, operating empty weight, and payload weight of the base aircraft.
File Size	477177
Page Count	10
File Format	PDF
Alternate Webpage(s)	http://archive.org/details/NASA_NTRS_Archive_20150016906
Archival Resource Key	ark:/13960/t0zp91q51
Language	English
Publisher Date	2015-07-27
Access Restriction	Open
Subject Keyword	Electronics And Electrical Engineering Aircraft Propulsion And Power Functional Design Specifications Costs Systems Engineering Turbogenerators Electric Power Power Efficiency Payloads Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science
Content Type	Text
Resource Type	Article

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