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Distribution of debris cloud caused by hypervelocity impact on AL-foam shield

  • Tsinghua University

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

Abstract

It's important to improve and optimize the shields used to protect the manned elements against impacts of micro-meteoroids and orbital debris. Tests have identified that metallic foams have a good shielding performance against M/OD hypervelocity impact, so metallic foams may play a key role in the structural design of manned spacecraft and satellite in the future. To investigate the distribution of debris clouds caused by impact on Al-foam shields compared to solid aluminum, numerical simulations were carried out in the velocity range of 3-9km/s at normal incidence angle. The distributions of mass and kinetic energy of debris cloud were obtained at different angles. The mass distribution of debris cloud caused by impact on Al-foam bumper shows two peaks at different velocities within 0-45 degrees. While the kinetic energy distribution of debris cloud shows only one peak within 0-15 degrees. The mass and kinetic energy of debris cloud caused by impact on Al-foam bumper are more dispersive at higher velocities than those of solid aluminum bumper. This feature will help to decrease the risk of spacecrafts against space debris with high speed.

Original languageEnglish
Title of host publication60th International Astronautical Congress 2009, IAC 2009
Pages1896-1901
Number of pages6
StatePublished - 2009
Event60th International Astronautical Congress 2009, IAC 2009 - Daejeon, Korea, Republic of
Duration: 12 Oct 200916 Oct 2009

Publication series

Name60th International Astronautical Congress 2009, IAC 2009
Volume3

Conference

Conference60th International Astronautical Congress 2009, IAC 2009
Country/TerritoryKorea, Republic of
CityDaejeon
Period12/10/0916/10/09

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