@article{oai:jaxa.repo.nii.ac.jp:00031200,
 author = {TAMURA, Hideki and UEDA, Keiji and USUI, Toshichika and SAWAOKA, Akira B.},
 journal = {The Institute of Space and Astronautical Science report. S.P. : Proceedings of the Workshop on Space Debris May 11, 1989 at ISAS Conference Hall},
 month = {Mar},
 note = {For the hypervelocity impact simulation of micrometeoroids on a space station, a plasma accelerator was constructed and tested to achieve projectile velocity of 10 km/s. Then the morphology of craters on an aluminum alloy target was investigated. The dual element shield structure consisting of aluminum alloy was tested up to 5 km/s impact. The morphology of impact area and the new technique of projectile emission was also reported., 資料番号: SA0033441000},
 pages = {21--29},
 title = {Projectile Hypervelocity Impact Simulation},
 volume = {11},
 year = {1990}
}