Computational Design of Metal–Fabric Orbital Debris Shielding-Reference-Cited by-同舟云学术

Computational Design of Metal–Fabric Orbital Debris Shielding

Published:2017-09 Issue:5 Volume:54 Page:1060-1067
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

Fahrenthold Eric P.¹

Affiliation:

1. University of Texas, Austin, Texas 78712

Funder

NASA Space Johnson Center

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.A33736

Reference26 articles.

1. Enhanced meteoroid and orbital debris shielding

2. Simulation of Orbital Debris Impact on Porous Ceramic Tiles

3. KalinskiM. E. “Hypervelocity Impact Analysis of International Space Station Whipple and Enhanced Stuffed Whipple Shields,” Master of Science Thesis, Naval Postgraduate School, Monterey, CA, Dec. 2004.

4. Scale modeling of hypervelocity impact

5. A kernel free particle-finite element method for hypervelocity impact simulation

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