Re: Titanium in the Shuttle

metalmorphosis_at_caverock.net.nz
Date: 03/27/05


Date: 27 Mar 2005 13:36:30 -0800


kitplane01@gmail.com wrote:
> <kitplan...@gmail.com> wrote:
> >A titanium structure would weigh less...
>
> No, substantially more -- NASA estimated an extra 2t -- although that
> would be more than made up by lighter thermal protection.
>
> >NASA did study this option. Why did they pick aluminum? Was it
just
> >the cost of titanium fabrication.
>
> Why would a titanium structre weight 2 tons *more* than an aluminum
> one?Titanium has a higher strength/weight ratio, and although
aluminum
> has a better stiffness/weight ration, that does not seem as relevent.
> I would expect a titanium wing to weigh less, be stronger, but flex
> more.

Flexing wing might be a bit of a bitch when it comes to the heat sheild
tiles..... load comes on, gaps open up, hot gases get in...... ???



Relevant Pages

  • Re: Titanium in the Shuttle
    ... >>NASA did study this option. ... Why did they pick aluminum? ... >>the cost of titanium fabrication. ... > I would expect a titanium wing to weigh less, be stronger, but flex ...
    (sci.space.tech)
  • Re: The Cold Equations
    ... I don't suppose you could produce a single citation of NASA ... > NASA pointed out, probably accurately, that if titanium had been used ... Aluminum melts at about 1000 deg. F., ... > steel' they were considering is uncertain. ...
    (sci.space.shuttle)