Model improvement for low-velocity collision possible in space

H. Hata, Y. Kurakazu, Y. Akahoshi, Toshiya Hanada, T. Yasaka, S. Harada

Research output: Contribution to journalArticlepeer-review

3 Citations (Scopus)

Abstract

We have conducted research related to space debris issues, including impact experiments associated with visualization of fragment creation processes. However, we aim at those phenomena in the geosynchronous regime where the impact velocity is far lower than hypervelocity. The research purpose is to understand dispersion properties of newly created fragments to be used in the eventual orbital dispersion and debris population models. At Kyushu University, the experiments had been carried out up to velocity of 300m/s so far. However, if debris in geostationary transfer orbits should be taken into consideration, the maximum impact velocity on geostationary satellites will become up to 1500 m/s. Therefore, the experiment in 300-1500 m/s is planed to be conducted using the Two-Stage Light Gas Gun at Kyushu Institute of Technology. The similarities and differences in the experimental results from Kyushu University and Kyushu Institute of Technology are discussed.

Original languageEnglish
Pages (from-to)323-332
Number of pages10
JournalInternational Journal of Impact Engineering
Volume29
Issue number1-10
DOIs
Publication statusPublished - Dec 1 2003

All Science Journal Classification (ASJC) codes

  • Civil and Structural Engineering
  • Automotive Engineering
  • Aerospace Engineering
  • Safety, Risk, Reliability and Quality
  • Ocean Engineering
  • Mechanics of Materials
  • Mechanical Engineering

Fingerprint Dive into the research topics of 'Model improvement for low-velocity collision possible in space'. Together they form a unique fingerprint.

Cite this