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Originally Posted by chrisbec I would venture to say that one made from aluminum would have more than enough strength... |
You may be right, but it also depends on which aluminum that is used. We have done strength analysis using a 6000-series (do not remember the exact one) of aluminum, and I did not take the chance of using it given this particular design.
E.g. the 6061 alloy has tensile strength of 310 MPa.
Using aircraft aluminum (the term aircraft aluminium or aerospace aluminium usually refers to 7075) is another option. The 7075-O grade has a tensile strength of 276 MPa. The 7075-T6 has a tensile strength of 510 - 538 MPa.
The Titanium planned to use here (Grade 5) has a tensile strength of 1000 MPa.
Better safe than sorry...