Projectile Shape Effects in Hypervelocity Impact of Honeycomb-Core Sandwich Structures-Reference-Cited by-同舟云学术

Projectile Shape Effects in Hypervelocity Impact of Honeycomb-Core Sandwich Structures

Published:2022-01 Issue:1 Volume:35 Page:04021112
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Aslebagh Reihaneh¹,Cherniaev Aleksandr²^ORCID

Affiliation:

1. Research Assistant, Dept. of Mechanical, Automotive and Materials Engineering, Univ. of Windsor, 401 Sunset Ave., Windsor, ON, Canada N9B 3P4.

2. Assistant Professor, Dept. of Mechanical, Automotive and Materials Engineering, Univ. of Windsor, 401 Sunset Ave., Windsor, ON, Canada N9B 3P4 (corresponding author). ORCID: .

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Link

http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29AS.1943-5525.0001365

Reference32 articles.

1. A Modular Design Concept For Small Satellites

2. Weight-Efficiency of Conventional Shielding Systems in Protecting Unmanned Spacecraft from Orbital Debris

3. Hypervelocity impact tests and simulations of single whipple bumper shield concepts at 10km/s

4. Design and performance equations for advanced meteoroid and debris shields

5. Christiansen, E. L. 2009. Handbook for designing MMOD protection: NASA JSC-64399. Houston: National Aeronautics and Space Administration.

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