Impact Characterization of Earth Entry Vehicle for Terminal Landing (on Soil)
In order to more accurately predict loads subjected to the EEV (Earth Entry Vehicle) upon impact with a variety of materials, finite element simulations of soil/EEV impact were created using the program LS-DYNA. Various modeling techniques were analyzed for accuracy through comparison with physical...
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ndltd-VTETD-oai-vtechworks.lib.vt.edu-10919-877272020-09-29T05:48:21Z Impact Characterization of Earth Entry Vehicle for Terminal Landing (on Soil) Shorts, Daniel Calvert Mechanical Engineering Bayandor, Javid Battaglia, Francine Perino, Scott Victor Mars Sample Return Earth Entry Vehicle Soil Impact Finite Element Analysis In order to more accurately predict loads subjected to the EEV (Earth Entry Vehicle) upon impact with a variety of materials, finite element simulations of soil/EEV impact were created using the program LS-DYNA. Various modeling techniques were analyzed for accuracy through comparison with physical test data when available. Through variation of numerical methods, mesh density, and material definition, an accurate and numerically efficient representation of physical data has been created. The numerical methods, Lagrangian, arbitrary Lagrangian-Eulerian (ALE), and spherical particle hydrodynamics (SPH) are compared to determine their relative accuracy in modeling soil deformation and EEV acceleration. Experimentally validated soil material parameters and element formulations were then used in parametric studies to gain a perspective on effects of EEV mass and geometry on its maximum acceleration across varying soil moisture content. Additionally, the effects of EEV orientation, velocity, and impact material were explored. Multi-material arbitrary Lagrangian-Eulerian (MMALE) formulation possess the most effective compromise between its ability to: accurately display qualitative soil behavior, accurately recreate empirical test data, be easily utilized in parametric studies, and to maintain simulation stability. EEV acceleration can be minimized through increase of EEV mass (with constant geometry), allowing for maximum penetration depth, and longest deceleration time. A critical orientation was discovered at 30⁰ from normal, such that maximum EEV surface area impacts the soil surface instantaneously, resulting in maximum acceleration. Off-nominal impact with concrete is predicted to increase acceleration by up to 630% from impact with soil. MS 2019-02-20T07:00:28Z 2019-02-20T07:00:28Z 2017-08-28 Thesis vt_gsexam:12578 http://hdl.handle.net/10919/87727 In Copyright http://rightsstatements.org/vocab/InC/1.0/ ETD application/pdf Virginia Tech |
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Mars Sample Return Earth Entry Vehicle Soil Impact Finite Element Analysis |
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Mars Sample Return Earth Entry Vehicle Soil Impact Finite Element Analysis Shorts, Daniel Calvert Impact Characterization of Earth Entry Vehicle for Terminal Landing (on Soil) |
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In order to more accurately predict loads subjected to the EEV (Earth Entry Vehicle) upon impact with a variety of materials, finite element simulations of soil/EEV impact were created using the program LS-DYNA. Various modeling techniques were analyzed for accuracy through comparison with physical test data when available. Through variation of numerical methods, mesh density, and material definition, an accurate and numerically efficient representation of physical data has been created. The numerical methods, Lagrangian, arbitrary Lagrangian-Eulerian (ALE), and spherical particle hydrodynamics (SPH) are compared to determine their relative accuracy in modeling soil deformation and EEV acceleration. Experimentally validated soil material parameters and element formulations were then used in parametric studies to gain a perspective on effects of EEV mass and geometry on its maximum acceleration across varying soil moisture content. Additionally, the effects of EEV orientation, velocity, and impact material were explored.
Multi-material arbitrary Lagrangian-Eulerian (MMALE) formulation possess the most effective compromise between its ability to: accurately display qualitative soil behavior, accurately recreate empirical test data, be easily utilized in parametric studies, and to maintain simulation stability. EEV acceleration can be minimized through increase of EEV mass (with constant geometry), allowing for maximum penetration depth, and longest deceleration time. A critical orientation was discovered at 30⁰ from normal, such that maximum EEV surface area impacts the soil surface instantaneously, resulting in maximum acceleration. Off-nominal impact with concrete is predicted to increase acceleration by up to 630% from impact with soil. === MS |
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Mechanical Engineering |
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Mechanical Engineering Shorts, Daniel Calvert |
author |
Shorts, Daniel Calvert |
author_sort |
Shorts, Daniel Calvert |
title |
Impact Characterization of Earth Entry Vehicle for Terminal Landing (on Soil) |
title_short |
Impact Characterization of Earth Entry Vehicle for Terminal Landing (on Soil) |
title_full |
Impact Characterization of Earth Entry Vehicle for Terminal Landing (on Soil) |
title_fullStr |
Impact Characterization of Earth Entry Vehicle for Terminal Landing (on Soil) |
title_full_unstemmed |
Impact Characterization of Earth Entry Vehicle for Terminal Landing (on Soil) |
title_sort |
impact characterization of earth entry vehicle for terminal landing (on soil) |
publisher |
Virginia Tech |
publishDate |
2019 |
url |
http://hdl.handle.net/10919/87727 |
work_keys_str_mv |
AT shortsdanielcalvert impactcharacterizationofearthentryvehicleforterminallandingonsoil |
_version_ |
1719347045068701696 |