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                                       Details for article 2 of 5 found articles
 
 
  Hole size and crack length models for spacecraft walls under oblique hypervelocity projectile impact
 
 
Title: Hole size and crack length models for spacecraft walls under oblique hypervelocity projectile impact
Author: Schonberg, William P.
Appeared in: Aerospace science and technology
Paging: Volume 3 (1999) nr. 7 pages 11 p.
Year: 1999
Contents:
Publisher: Éditions scientifiques et médicales Elsevier SAS
Source file: Elektronische Wetenschappelijke Tijdschriften
 
 

                             Details for article 2 of 5 found articles
 
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