@inproceedings{4af1f56bf25b4755842062110154c37e,
title = "Dynamic high temperature and pressure characterization of an inconel honeycomb impact attenuator",
abstract = "Possible mission concepts for a Venus lander include a passive landing gear system that dissipates the lander{\textquoteright}s kinetic energy during the landing event. In order to demonstrate the performance of a metallic honeycomb crushable that could be integrated into the land- ing system of a Venus lander, high temperature and pressure drop tests are performed. Accelerometer data is used to quantify the performance of the crushable under different conditions, and is used to relate the observed performance of the crushable to the predicted material degradation at elevated temperatures.",
author = "Sly, {Jacqueline R.} and Elham Maghsoudi and Pauken, {Michael T.} and Aubuchon, {Patricia J.} and Dunkl, {John M.} and Kochk, {Justin R.} and Hyeong, {Jae Lee} and Jason Rabinovitch",
note = "Publisher Copyright: {\textcopyright} 2018, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.; AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 2018 ; Conference date: 08-01-2018 Through 12-01-2018",
year = "2018",
doi = "10.2514/6.2018-1444",
language = "English",
isbn = "9781624105326",
series = "AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 2018",
booktitle = "AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials",
}