Numerical Analysis of Hyper Velocity Impact on quasi-isotropic carbon fiber reinforced polymer laminates-Reference-Cited by-同舟云学术

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Numerical Analysis of Hyper Velocity Impact on quasi-isotropic carbon fiber reinforced polymer laminates

Published:2023-11 Issue: Volume: Page:
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Pai Anand^ORCID,Rodriguez-Millan Marcos,Nishida Masahiro,Su Ziyi,Shenoy B Satish

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference28 articles.

1. Advanced meteoroid and debris shielding concepts;Christiansen;Orbital Debris Conf. Tech. Issues Futur. Dir.,1990

2. Orbital missions safety – A survey of kinetic hazards;Adushkin;Acta Astronaut,2016

3. Physical and mathematical models for space objects breakup and fragmentation in hypervelocity collisions;Smirnov;Acta Astronaut,2020

4. Effects of high-speed impacts on CFRP plates for space applications;Francesconi;Adv. Sp. Res.,2012

5. An engineering model to describe fragments clouds propagating inside spacecraft in consequence of space debris impact on sandwich panel structures;Francesconi;Acta Astronaut,2015

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1. Review of bumper materials for spacecraft shield against orbital debris hypervelocity impact;Defence Technology;2024-09

2. Computational studies on hyper velocity impact of spherical projectiles on whipple shield with hybrid Newtonian fluid-filled core;Acta Astronautica;2024-07

3. Review on hypervelocity impact of advanced space debris protection shields;Thin-Walled Structures;2024-07

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