Predicting the Rupture of a COPV Impacted by a High-Speed Orbital Debris Particle: Including the Effects of Temperature and COPV Contents-Reference-Cited by-同舟云学术

Predicting the Rupture of a COPV Impacted by a High-Speed Orbital Debris Particle: Including the Effects of Temperature and COPV Contents

Published:2021-05 Issue:3 Volume:34 Page:06021002
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Schonberg William P.¹

Affiliation:

1. Professor, Dept. of Civil, Architectural, and Environmental Engineering, Missouri Univ. of Science and Technology, Rolla, MO 65409.

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.1943-5525.0001248

Reference17 articles.

1. Davis B. A. E. L. Christiansen J. E. Miller and T. B. Yoder. 2019. “Hypervelocity impact of composite overwrap pressure vessels.” In Proc. 1st Int. Orbital Debris Conf. Houston: Lunar and Planetary Institute.

2. Hypervelocity impact testing of a pressurized composite overwrapped pressure vessel and comparison to numerical analysis

3. Hassin J. K. Pfaab C. Puillet J. Limido J. L. Lacome and P. Hereil. 2015. “Hypervelocity impacts on composite overwrapped pressurized vessels.” In Proc. DYNCOMP 2015. Villeurbanne France: Centre pour la Communication Scientifique Directe.

4. Hypervelocity Impact of Aluminum Projectiles Against Pressurized Aluminum-composite Vessel

5. Lear D. M. E. L. Christiansen and J. L. Hyde. 2019. “Bumper: A tool for analyzing spacecraft micrometeoroid and orbital debris risk.” In Proc. 1st Int. Orbital Debris Conf. Washington DC: The National Aeronautics and Space Administration.

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