With the swift advancement of aerospace, shipbuilding and engineering, the significance of
sandwich structures with cellular cores is becoming increasingly prominent due to their multi …

Spacecraft that are launched to operate in Earth orbit are susceptible to impacts by
meteoroids and pieces of orbital debris (MMOD). The effect of a MMOD particle impact on a …

This paper presents the results of preliminary empirical testing and numerical modelling
carried out to demonstrate the effectiveness of using a harpoon in an ADR application …

In this paper, the honeycomb sandwich panel (HSP) reinforced with bi-layer Ceramic
(B4C)/Aluminum (Al7075-T6) facesheets is proposed to be used as a shield for spacecraft …

Current spacecraft micrometeoroid and orbital debris impact risk assessments utilize semi-
empirical equations to describe the protection afforded by a spacecraft component (eg …

A series of 66 hypervelocity impact experiments have been performed to assess the
potential of various materials (aluminium, titanium, copper, stainless steel, nickel …

In keeping with the tradition of the Hypervelocity Impact Society, this paper is a written
version of the keynote address I presented at the start of 2015 Hypervelocity Impact …

This software implements penetration limit equations for common micrometeoroid and
orbital debris (MMOD) shield configurations, windows, and thermal protection systems …

Space debris represent a threat to satellites in orbit around Earth. In the case of impact,
satellites can be subjected to damage spanning from localized craterization to subsystem …

多孔夹芯结构是一类由薄而刚硬的面板和多孔材料芯材构成的复合结构, 具有高比刚度,
高比强度, 缓冲吸能效果优异, 可设计性强等特性, 在航空航天, 交通运输, 结构防护等诸多领域 …