Experimental Evaluation of the Canadarm2 Residual Flexural Strength After an Orbital Debris Impact
European Conference; 13th, Spacecraft structures, materials & environmental testing; 13th European conference on spacecraft structures, materials & environmental testing; proceedings; editor: L. Ouwehand ; 2014 ; Braunschweig, Germany
2014-01-01
143 pages
Held in e-store (RMS)
Aufsatz (Konferenz)
Englisch
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The orbital debris hypervelocity impact effects
AIAA | 2005
|Online Contents | 1998
Online Contents | 1993
NTRS | 1985
|NTIS | 1985
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