Space/Science — HabitableZone

Space/Science » in reply to re: SR-71 doesnt face re-entry temps...

Correct... Titanium can not be used on a reentering vehicle's leading edge

R.L. is quite correct that titanium can not be used on a reentering vehicle's leading edge. I mentioned in another post that reinforced carbon carbon (RCC) or an exotic material like hafnium diboride would have to be used for the leading edges.

Years ago I did the calculation so my memory is hazy about this but I vaguely remember the peak Mach number for an uncooled titanium leading edge at 110,000 feet is around Mach = 3.5 . This was one of the things that limited the SR-71's peak Mach number. Of course the leading edges can be regenerative cooled and that would permit a higher Mach number. There was idle speculation that Aurora flew with regeneratively cooled titanium leading edges.

Gary

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