Critical fracture of Space Station modules following orbital debris penetration-Reference-Cited by-同舟云学术

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Critical fracture of Space Station modules following orbital debris penetration

Published:1996-08-22 Issue: Volume: Page:
ISSN:
Container-title:Space Programs and Technologies Conference
language:
Short-container-title:

Author:

Lutz Bernard¹,Williamsen Joel²

Affiliation:

1. Meyer Analytics, Warrenton, VA

2. NASA, Marshall Space Flight Center, Huntsville, AL

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1996-4362

Reference7 articles.

1. A finite line crack in a pressurized spherical shell

2. Jeong,D.Y.andlong,P. "NonlinearBulging FactorBasedonR-CurveData,"NASAConference Publication 3274,Part 1,1994.

3. A Path Independent Integral and the Approximate Analysis of Strain Concentration by Notches and Cracks

Cited by 2 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. Progress in Lightweight Design Methods for Large-Size Panel Structures in Manned Pressurized Capsules;Applied Sciences;2023-07-26

2. Research on Crack Stop Characteristics of Integrally Stiffened Structure for Spacecraft Pressured Modules;Advances in Astronautics Science and Technology;2022-06-26

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