| http://www.w3.org/ns/prov#value | - FIG. 1 is a chart comparing the specific strengths of common aerospace materials with the specific strengths of a 5 layer laminate having 3 plies of 0.010 Timetal?? 15-3 sheet and 2 layers of unidirectional 1M8 carbon/epoxy fiber that are 0.030 thick each.
|
