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  4. Optical fragment tracking in hypervelocity impact experiments
 
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2019
Journal Article
Title

Optical fragment tracking in hypervelocity impact experiments

Abstract
In-orbit impacts between satellites and space debris lead to varying degrees of fragmentation, ranging anywhere from minor damage to complete breakups. In this paper, we describe an experimental measurement approach for studying fragmentation caused by hypervelocity impact in the laboratory. We investigate impacts on thin aluminum bumper plates with the goal of measuring individual fragment velocities and sizes generated by hypervelocity impact. The experimental setup, commonly used in fluid dynamics for Particle Tracking Velocimetry, consists of using a laser plane and high-speed video camera to track the motion of debris fragments. We describe the fragment tracking algorithm and demonstrate its ability to determine fragment velocity and sizes in specific hypervelocity impact experiments performed at Fraunhofer EMI. The measurement technique enables quantitative data, at an unprecedented level of detail, to be measured from hypervelocity impact fragmentation experiments in the lab, which can be applied to understanding the effects of satellite collisions and improving breakup models.
Author(s)
Watson, Erkai  
Fraunhofer-Institut für Kurzzeitdynamik Ernst-Mach-Institut EMI  
Gulde, Max  
Fraunhofer-Institut für Kurzzeitdynamik Ernst-Mach-Institut EMI  
Kortmann, Lukas  
Fraunhofer-Institut für Kurzzeitdynamik Ernst-Mach-Institut EMI  
Higashide, Masumi
Research and Development Directorate, Japan
Schäfer, Frank  
Fraunhofer-Institut für Kurzzeitdynamik Ernst-Mach-Institut EMI  
Hiermaier, Stefan  
Fraunhofer-Institut für Kurzzeitdynamik Ernst-Mach-Institut EMI  
Journal
Acta astronautica  
DOI
10.1016/j.actaastro.2018.11.036
Language
English
Fraunhofer-Institut für Kurzzeitdynamik Ernst-Mach-Institut EMI  
Keyword(s)
  • hypervelocity impact

  • fragmentation

  • particle tracking

  • satellite breakup

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