[p-1] r) Space Environment and Debris

[2023-r-23] Applicability of Conventional Ballistic Limit Equation to Titanium Alloy Curved Plate and Energy Distribution of the Fragments after Perforation

*Hiroya Adachi¹, Masumi Higashide¹, Sayaka Suzuki¹, Hirohide Ikeda², Taiichi Nagata², Kumi Nitta² (1. Hosei Univ. Department of Mechanical Engineering, 2. JAXA)

Keywords:Space Debris, Hypervelocity Impact Test, Curved Panel, Fragments