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Design, Fabrication and Testing of a Crushable Energy Absorber for a Passive Earth Entry VehicleA conceptual study was performed to investigate the impact response of a crushable energy absorber for a passive Earth entry vehicle. The spherical energy-absorbing concept consisted of a foam-filled composite cellular structure capable of omni-directional impact-load attenuation as well as penetration resistance. Five composite cellular samples of hemispherical geometry were fabricated and tested dynamically with impact speeds varying from 30 to 42 meters per second. Theoretical crush load predictions were obtained with the aid of a generalized theory which accounts for the energy dissipated during the folding deformation of the cell-walls. Excellent correlation was obtained between theoretical predictions and experimental tests on characteristic cell-web intersections. Good correlation of theory with experiment was also found to exist for the more complex spherical cellular structures. All preliminary design requirements were met by the cellular structure concept, which exhibited a near-ideal sustained crush-load and approximately 90% crush stroke.
Document ID
20020051120
Acquisition Source
Langley Research Center
Document Type
Contractor Report (CR)
Authors
Kellas, Sotiris
(Veridian Systems Div. Fairfax, VA United States)
Corliss, James M.
Date Acquired
September 7, 2013
Publication Date
April 1, 2002
Subject Category
Launch Vehicles And Launch Operations
Report/Patent Number
NAS 1.26:211425
NASA/CR-2002-211425
Report Number: NAS 1.26:211425
Report Number: NASA/CR-2002-211425
Funding Number(s)
PROJECT: RTOP 896-30-00
CONTRACT_GRANT: GS-32F-4503G
CONTRACT_GRANT: NASA Order L-13998
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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