Investigation of penetrant power of bullet and magnetic field of railgun

سال انتشار: 1397
نوع سند: مقاله کنفرانسی
زبان: انگلیسی
مشاهده: 490

فایل این مقاله در 5 صفحه با فرمت PDF قابل دریافت می باشد

استخراج به نرم افزارهای پژوهشی:

لینک ثابت به این مقاله:

شناسه ملی سند علمی:

CMTS02_007

تاریخ نمایه سازی: 29 تیر 1398

چکیده مقاله:

The shielding of spacecraft and satellites from the impacts of space debris partides of millimeter size is an important problem in space industry and exploration. As a rule, these particles have irregular shapes; therefore, their impact leads to different consequences from the impact of spherical particles. The goal of our study was to reveal spedfic features in the hypervelocity impact of cubic impactors on thin metal and polymer plates (elements of multilayer spacecraft and satellite shielding, which is known as the Whipple shield ).

کلیدواژه ها:

نویسندگان

Hossein riazi

Defense Engineer, Imam Ali University, Tehran, Iran

nikzad nazari

Defense Engineer, Imam Ali University, Tehran, Iran

erfan cholaki

Department of Physics, Faculty of Science, Islamic Azad University of Kermanshah branch, Kermanshah,

Shahryar heidari

Department of Management Specialized Defense Engineering, Faculty of Management, Imam Ali University, Tehran, Iran