An Internal Effects Model for a Habitable Spacecraft Module Perforated by an Orbital Debris Particle
Hypervelocity shielding workshop ; 1998 ; Galveston, TX
Hypervelocity shielding workshop ; 121-130
01.01.1999
10 pages
Aufsatz (Konferenz)
Englisch
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Internal Effects Model for Spacecraft Modules Perforated by Orbital Debris
Online Contents | 1997
|British Library Conference Proceedings | 1996
|Onset of petalling in a thin spacecraft wall perforated by an orbital debris particle
SAGE Publications | 1998
|