Mesh double-bumper shield: A low-weight alternative for spacecraft meteoroid and orbital debris protection-Reference-Cited by-同舟云学术

Mesh double-bumper shield: A low-weight alternative for spacecraft meteoroid and orbital debris protection

Published:1993-01 Issue:1-4 Volume:14 Page:169-180
ISSN:0734-743X
Container-title:International Journal of Impact Engineering
language:en
Short-container-title:International Journal of Impact Engineering

Author:

Christiansen Eric L.,Kerr Justin H.

Publisher

Elsevier BV

Subject

Mechanical Engineering,Mechanics of Materials,Ocean Engineering,Safety, Risk, Reliability and Quality,Aerospace Engineering,Automotive Engineering,Civil and Structural Engineering

Reference13 articles.

1. Hydrocode Simulations in Support of the Development of Advanced Shielding Concepts. RDA Associates;Alme,1991

2. Hydrocode Simulations of the Multi-Shock Meteoroid and Debris Shield;Alme,1991

3. Evaluation of Space Station Meteoroid/Debris Shielding Materials;Christiansen;Eagle Engineering Report No. 87-163,1987

4. Advanced Meteoroid and Debris Shielding Concepts. AIAA Paper No. 90-1336;Christiansen,1990

5. Augmentation of Orbital Debris Shielding for Space Station Freedom. AIAA Pa.per No. 90-3665;Christiansen,1990

Cited by 76 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. A review of shielding systems for protecting off-earth structures from micrometeoroid and orbital debris impact;Acta Astronautica;2024-10

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

3. Numerical simulation study on mesoscopic metallic foam core sandwich panels under hypervelocity impact;Thin-Walled Structures;2024-02

4. Design and Evaluation of Additively Manufactured Polyetherimide Orbital Debris Shielding for Spacecraft;2024

5. A Light Dust Shield, Including Aerogel, for Space Applications: The Study Case for Disc – Part of the Payload Selected for the Esa/Comet Interceptor Space Mission;2024