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Overview of the Transport Rotorcraft Airframe Crash Testbed (TRACT) Full Scale Crash TestsThe Transport Rotorcraft Airframe Crash Testbed (TRACT) full-scale tests were performed at NASA Langley Research Center's Landing and Impact Research Facility in 2013 and 2014. Two CH-46E airframes were impacted at 33-ft/s forward and 25-ft/s vertical combined velocities onto soft soil, which represents a severe, but potentially survivable impact scenario. TRACT 1 provided a baseline set of responses, while TRACT 2 included retrofits with composite subfloors and other crash system improvements based on TRACT 1. For TRACT 2, a total of 18 unique experiments were conducted to evaluate Anthropomorphic Test Devices (ATD) responses, seat and restraint performance, cargo restraint effectiveness, patient litter behavior, and activation of emergency locator transmitters and crash sensors. Combinations of Hybrid II, Hybrid III, and ES-2 ATDs were placed in forward and side facing seats and occupant results were compared against injury criteria. The structural response of the airframe was assessed based on accelerometers located throughout the airframe and using three-dimensional photogrammetric techniques. Analysis of the photogrammetric data indicated regions of maximum deflection and permanent deformation. The response of TRACT 2 was noticeably different in the horizontal direction due to changes in the cabin configuration and soil surface, with higher acceleration and damage occurring in the cabin. Loads from ATDs in energy absorbing seats and restraints were within injury limits. Severe injury was likely for ATDs in forward facing passenger seats.
Document ID
20160006501
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Annett, Martin
(NASA Langley Research Center Hampton, VA, United States)
Littell, Justin
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
May 23, 2016
Publication Date
November 17, 2015
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NF1676L-21540
Report Number: NF1676L-21540
Meeting Information
Meeting: Aerospace Structural Impact Dynamics International Conference (ASIDIC) 2015
Location: Seville
Country: Spain
Start Date: November 17, 2015
End Date: November 19, 2015
Sponsors: Airbus Industrie, NASA Headquarters
Funding Number(s)
WBS: WBS 845953.01.03.02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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