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)
Conference paper
English
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Online Contents | 1993
The orbital debris hypervelocity impact effects
AIAA | 2005
|NTRS | 1985
|Online Contents | 1998
Residual Strength of CFRP Tubes Subjected to Hypervelocity Debris Impact
British Library Conference Proceedings | 1994
|