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Stability, Transient Response, Control, and Safety of a High-Power Electric Grid for Turboelectric Propulsion of AircraftThis document contains the deliverables for the NASA Research and Technology for Aerospace Propulsion Systems (RTAPS) regarding the stability, transient response, control, and safety study for a high power cryogenic turboelectric distributed propulsion (TeDP) system. The objective of this research effort is to enumerate, characterize, and evaluate the critical issues facing the development of the N3-X concept aircraft. This includes the proposal of electrical grid architecture concepts and an evaluation of any needs for energy storage.
Document ID
20140000336
Acquisition Source
Glenn Research Center
Document Type
Contractor Report (CR)
Authors
Armstrong, Michael (Rolls-Royce North American Technologies, Inc. Indianapolis, IN, United States)
Ross, Christine (Rolls-Royce North American Technologies, Inc. Indianapolis, IN, United States)
Phillips, Danny (Rolls-Royce North American Technologies, Inc. Indianapolis, IN, United States)
Blackwelder, Mark (Rolls-Royce North American Technologies, Inc. Indianapolis, IN, United States)
Date Acquired
January 22, 2014
Publication Date
June 1, 2013
Subject Category
Aerodynamics
Report/Patent Number
E-18658
NASA/CR-2013-217865
Funding Number(s)
CONTRACT_GRANT: NNC10BA14B
TASK: NNC11TA51T
WBS: WBS 432938.11.01.03.02.02.16
Distribution Limits
Public
Copyright
Public Use Permitted.

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