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
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
The whole thread (44 posts)
- Mike Griffin's road map to Mars
- I think rocket technology is about as good as it's going to get
- Other good points
- I agree
- The 30+ years hasn't been a complete waist.
- re: I agree
- Could the shuttles be redesigned?
- I agree
