DOI

  • S. A. Poniaev
  • R. O. Kurakin
  • A. I. Sedov
  • S. V. Bobashev
  • B. G. Zhukov
  • A. F. Nechunaev

The experimental studies of the process of hypervelocity (up to 6 km/s) impact of a mm-size projectile on a thin aluminum plate is described. The numerical simulation of this process is presented. The data on the evolution, structure, and composition of the debris cloud formed as a result of the impact are reported. Basic specific features of the debris cloud formation are revealed.

Язык оригиналаанглийский
Страницы (с-по)26-33
Число страниц8
ЖурналActa Astronautica
Том135
DOI
СостояниеОпубликовано - 1 июн 2017

    Предметные области Scopus

  • Авиакосмическая техника

ID: 7613552