TY - GEN
T1 - Overview of Hypervelocity Response of Space Structures to Oblique Impacts
AU - Stokes, Sean
AU - Bayandor, Javid
N1 - Publisher Copyright: © 2023, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
PY - 2023
Y1 - 2023
N2 - Hypervelocity physics are relatively well understood for normal impact events. There exist numerous high-quality radiographs of debris cloud development at 90° incidence, but experimental studies of similar quality are not available for oblique impact scenarios. While the shock pressures present in hypervelocity impact cause extreme deformation as well as potential melt and vaporization of space structures, the projectile trajectory causes different response that is not well understood. This work utilizes a meshless, discretized particle method to model debris cloud development for oblique impact, discerning important characteristics present in both thick and thin bumper plates in hypervelocity.
AB - Hypervelocity physics are relatively well understood for normal impact events. There exist numerous high-quality radiographs of debris cloud development at 90° incidence, but experimental studies of similar quality are not available for oblique impact scenarios. While the shock pressures present in hypervelocity impact cause extreme deformation as well as potential melt and vaporization of space structures, the projectile trajectory causes different response that is not well understood. This work utilizes a meshless, discretized particle method to model debris cloud development for oblique impact, discerning important characteristics present in both thick and thin bumper plates in hypervelocity.
UR - https://www.scopus.com/pages/publications/85191249126
U2 - 10.2514/6.2023-1111
DO - 10.2514/6.2023-1111
M3 - Conference contribution
SN - 9781624106996
T3 - AIAA SciTech Forum and Exposition, 2023
BT - AIAA SciTech Forum and Exposition, 2023
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - AIAA SciTech Forum and Exposition, 2023
Y2 - 23 January 2023 through 27 January 2023
ER -