Hypervelocity impact on flexible curable composites and pure fabric layer bumpers for inflatable space structures

Author:

Kim YunHo,Choi Chunghyeon,Sathish Kumar Sarath Kumar,Kim Chun-Gon

Funder

National Research Foundation of Korea

Publisher

Elsevier BV

Subject

Civil and Structural Engineering,Ceramics and Composites

Reference27 articles.

1. International Space Station Imagery, NASA, ISS022-E-020895.

2. Inflatable composite habitat structures for lunar and mars exploration;Cadogan;Acta Astronaut,1999

3. Flexible and deployable meteoroid/debris shielding for spacecraft;Christiansen;Int J Impact Eng,1999

4. Di Capua M, Akin DL Dr., Davis K. Design, development, and testing of an inflatable habitat element for NASA lunar analogue studies. In: 41st International conference on environmental systems 2011, ICES 2011; 2011. p. 1–20.

5. Bernasconi MC. Going elsewhere – adapting structures for use in space through rigidizing materials; 2006. p. 208–17.

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3. The Hypervelocity Impact Behavior and Energy Absorption Evaluation of Fabric;Polymers;2023-03-21

4. Hybrid interspaced and free-boundary aramid fabric back bumper for hypervelocity impact shielding system;International Journal of Impact Engineering;2023-01

5. Bibliography;Design and Fabrication of Large Polymer Constructions in Space;2023

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