[HTML][HTML] Non-polymer-matrix composite materials for space applications

M May, GD Rupakula, P Matura - Composites Part C: Open Access, 2020 - Elsevier
Abstract Space is a harsh environment creating many challenges for structural materials
used in space systems. Composite materials are one key enabler for space systems due to …

Orbital debris threat for space sustainability and way forward

A Murtaza, SJH Pirzada, T Xu, L Jianwei - IEEE access, 2020 - ieeexplore.ieee.org
Over the past 60 years, satellite technology has demonstrated its usefulness successfully.
However, this usefulness is at stake from a future point of view, due to the well-admitted …

Protecting Earth-orbiting spacecraft against micro-meteoroid/orbital debris impact damage using composite structural systems and materials: An overview

WP Schonberg - Advances in Space Research, 2010 - Elsevier
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 …

Measurements of freely-expanding plasma from hypervelocity impacts

N Lee, S Close, D Lauben, I Linscott, A Goel… - International Journal of …, 2012 - Elsevier
This paper details initial results from a study of electrical effects resulting from hypervelocity
impacts at a Van de Graaff dust accelerator. Iron particles between 10− 15 g and 10− 10 g in …

Internal-structure-model based simulation research of shielding properties of honeycomb sandwich panel subjected to high-velocity impact

P Liu, Y Liu, X Zhang - International Journal of Impact Engineering, 2015 - Elsevier
Honeycomb sandwich panel has been widely used in aerospace and aeronautic
engineering as load-bearing components. Cost-effective shielding structure can also be built …

An engineering model to describe fragments clouds propagating inside spacecraft in consequence of space debris impact on sandwich panel structures

A Francesconi, C Giacomuzzo, F Feltrin, A Antonello… - Acta Astronautica, 2015 - Elsevier
All spacecraft in Earth orbit are exposed to the risk of impact with micrometeoroids and
orbital debris. When such particles have enough energy to penetrate the hull of the vehicle …

Concept for a new light-gas gun type hypervelocity accelerator

R Putzar, F Schaefer - International Journal of Impact Engineering, 2016 - Elsevier
A new two-stage light-gas gun type accelerator was developed at Fraunhofer EMI. The
pumping stage is modified to create a single, elongated pressure pulse to act on the …

Satellite vulnerability to space debris–an improved 3D risk assessment methodology

L Grassi, F Tiboldo, R Destefanis, T Donath… - Acta Astronautica, 2014 - Elsevier
The work described in the present paper, performed as a part of the P 2 project, presents an
enhanced method to evaluate satellite vulnerability to micrometeoroids and orbital debris …

Computational methodology to predict satellite system-level effects from impacts of untrackable space debris

N Welty, M Rudolph, F Schäfer, J Apeldoorn… - Acta Astronautica, 2013 - Elsevier
This paper presents a computational methodology to predict the satellite system-level effects
resulting from impacts of untrackable space debris particles. This approach seeks to improve …

Characteristics of plasma generated by hypervelocity impact

W Song, J Li, J Ning - Physics of Plasmas, 2013 - pubs.aip.org
The characteristics of plasma generated by hypervelocity impact were studied through both
theoretical analysis and numerical simulation. Based on thermodynamics and statistical …