Titanium has about half the density of steel, which puts it between aluminum and steel. Ivan tells me that his titanium alloy is 6AL/4V, which is 6% aluminum and 4% vanadium. But that doesn't matter--all titanium alloys have about the same density. By the way, 6AL/4V is commonly used in aircraft and high-end titanium bicycles. Properly worked and heat-treated, it's as strong as hardened steel but at half the weight.TubaGrandad wrote:Do GW use a specific Titanium alloy which would increase the weight over aircraft grade stuff I'm thinking of? Am I missing something?
But it's only about half as stiff as steel, making its specific stiffness about the same as steel (and aluminum, for that matter). Stiffness, like density, is not significantly affected by alloy or hardening treatments.
Rick "thinking strength is unimportant, but modulus of elasticity is" Denney
Edit: I changed the alloy percentages above. I was confusing 6/4 with 3/2.5, both of which are are used in aircraft and high-end bikes. Ivan straightened me out.