Integrity assessment of the spacecraft subjected to the hypervelocity impact by ceramic and metal projectiles simulating space debris and micrometeoroids-Reference-Cited by-同舟云学术

Integrity assessment of the spacecraft subjected to the hypervelocity impact by ceramic and metal projectiles simulating space debris and micrometeoroids

Published:2010-10 Issue:1-3 Volume:173 Page:148-154
ISSN:0921-5107
Container-title:Materials Science and Engineering: B
language:en
Short-container-title:Materials Science and Engineering: B

Author:

Katayama Masahide,Takeba Atsushi,Nitta Kumi,Kawakita Shirou,Matsumoto Haruhisa,Kitazawa Yukihito

Publisher

Elsevier BV

Subject

Mechanical Engineering,Mechanics of Materials,Condensed Matter Physics,General Materials Science

Reference10 articles.

1. B.G. Cour-Palais, AIAA Hypervelocity Impact Conf. Paper No.69-372, 1969.

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

3. High-Velocity Impact Phenomena;McQueen,1970

4. J.H. Tillotson, Metallic equations of state for hypervelocity impact. GA-3216, General Atomic, CA, July 1962.

5. Extension of the Thomas-Fermi-Dirac Statistical Theory of the Atom to Finite Temperatures

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