Design and performance equations for advanced meteoroid and debris shields-Reference-Cited by-同舟云学术

Design and performance equations for advanced meteoroid and debris shields

Published:1993-01 Issue:1-4 Volume:14 Page:145-156
ISSN:0734-743X
Container-title:International Journal of Impact Engineering
language:en
Short-container-title:International Journal of Impact Engineering

Author:

Christiansen Eric L.

Publisher

Elsevier BV

Subject

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

Reference20 articles.

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

2. Hypervelocity Testing of Advanced Shielding for Spacecraft Against Impacts to 10 km/s;Boslough;Int. J. Impact Engng,1992

3. A New Hypervelocity Launcher (HVL) for Space Science Application;Chhablidis;AIAA Paper Number 92-1639,1992

4. Advanced Meteoroid and Debris Shielding Concepts;Christiansen,1990

5. Whipple Shield Sizing Equations;Christiansen;NASA JSC Memorandum SN3-91-19,1991

Cited by 204 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 Whipple shield ballistic limit equations;International Journal of Impact Engineering;2024-05

2. The pursuit of hypervelocities: A review of two-stage light gas gun aeroballistic ranges;International Journal of Impact Engineering;2024-03

3. Impact dynamic response of large aperture space deployable antenna supporting structures based on a dual-scale model;Thin-Walled Structures;2024-02

4. Selection of shaped charges parameters for producing aluminum particles with velocities in the range of 2.5–16 km/s;Defence Technology;2024-02

5. Influence of Whipple Shield Configuration on Hypervelocity Impact Resistance;AIAA SCITECH 2024 Forum;2024-01-04