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Technology Maturation Report for Damage Arresting Composites under the Environmentally Responsible Aviation ProjectThe goal of the NASA Environmentally Responsible Aviation (ERA) Project was to develop technologies that will lead to commercial aircraft that will burn less fuel and produce fewer emissions than the 2010 state of the art. The purpose of this Technology Maturation Report (TMR) is to summarize both the development and lessons learned for the Damage Arresting Composites (DAC) Demonstration and to summarize how the test results were used to predict the impact the Pultruded Rod Stitched Efficient Unitized Structure (PRSEUS) technology would have on future transport aircraft weights. The TMR includes the technical work plans for the DAC Demonstration for the six-year effort of the NASA ERA Project. System studies indicated that DAC would reduce structural weight by 20% for both hybrid wing body and tube and wing aircraft. A lighter vehicle requires less energy to fly so weight savings becomes reduced fuel burn. Additionally, the hybrid wing body configuration has improved lift-to-drag ratios compared to the tube and wing aircraft, further reducing fuel burn.
Document ID
20220015363
Acquisition Source
Langley Research Center
Document Type
Technical Memorandum (TM)
Authors
Dawn C Jegley
(Langley Research Center Hampton, Virginia, United States)
Jason A Corman
(Georgia Institute of Technology Atlanta, Georgia, United States)
Date Acquired
October 12, 2022
Publication Date
October 1, 2022
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NASA/TM-20220015363
Funding Number(s)
WBS: 278864.01.07.10.02
TASK: NNX10AM13H
CONTRACT_GRANT: NNL09AA00A
Distribution Limits
Public
Copyright
Use by or on behalf of the US Gov. Permitted.
Technical Review
NASA Technical Management
Keywords
carbon-epoxy
hybrid wing body
PRSEUS
weight savings
uncertainties
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