>> Russia Prepares Launch of New Space Shuttle
>>
[quoted text clipped - 9 lines]
> I would be very interested to know if they are using aluminum or titanium
> for Kliper.
> 1.) What was the material decision criteria? (e.g., influences from
> Columbia accident, cost, ease of fabrication of material, availability of
> metal).
When you look at the aerodynamic heating environment that an orbital
reentry takes place within, there's no structural reason to use
Titanium over Aluminum. The heat leves on the outside of the ship are
so high that both materiels will fail if the heat gets in. If you're
able to build a Thermal Protection System that works for Titanium,
It'll work for Aluminum, too. When you factor in the difficuly to
build and maintain a Titanium structure, and the new failure modes you
introduce by using Titanium, Aluminum looks like a more reasonable
choice.
(The SR-71 is able to use Ti over Al because it flies in an area (Mach
3-Mach 4) where it's too hot for Aluminum, and not yet too hot for Ti.
If you want to go faster than the upper Mach3-Mach 4 range, Titanium
won't cut it. That's why the X-15 was carged out of Iconel-X)
> 2.) Since titanium is more readily to Russia than the US, did this place a
> role in the decision?
It would, but that's only hte cost of the raw ore. Refining it,
smelting it, and machining it is still a gold-plated uhm - well, you
get the idea.

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Pete Stickney
A strong conviction that something must be done is the parent of many
bad measures. -- Daniel Webster
G.Beat - 16 Oct 2004 21:22 GMT
>>> Russia Prepares Launch of New Space Shuttle
>>>
[quoted text clipped - 28 lines]
> If you want to go faster than the upper Mach3-Mach 4 range, Titanium
> won't cut it. That's why the X-15 was carged out of Iconel-X)
When I read 1970 documents regarding decisions and compromises for the STS
design,
it appears that aluminum was selected due to:
1.) The difficulty in building & maintaining a titanium structure (from
SR-71 and aircraft mfg. experience) versus deeper experience with aluminum
for aerospace fabrication
2.) Supply and cost of titanium versus aluminum
>> 2.) Since titanium is more readily to Russia than the US, did this place
>> a
[quoted text clipped - 3 lines]
> smelting it, and machining it is still a gold-plated "uhm" - well, you
> get the idea.
It appears that previous aerospace fabrication experience is the primary
selection criteria, with cost a close second.
gb
Peter Stickney - 17 Oct 2004 04:03 GMT
>>>> Russia Prepares Launch of New Space Shuttle
>>>>
[quoted text clipped - 49 lines]
> It appears that previous aerospace fabrication experience is the primary
> selection criteria, with cost a close second.
What it basically comes down to is that to handndle teh heat loads of
an orbital reentry, you'd still ahve to use a serious Thermal
Protection System to keep the heat away from the structure. (As in teh
tiles & RCC - steel-burning hot on the outside, cool to the touch on
theinside.) The strength/temperature character of Ti isn't so much
better than Aluminum that it would make any difference They'll both
soften & fail equally well. (or poorly). If you're going to need teh
Super-Hyper TPS anyway, there's no need to complicate things by using
Ti.
Note that while the Russians have a lot of Ti in the ground, we've got
more experience making stuff out of it. (Although one has to really
wonder about the Blood level in the Alcohol System of whoever thought
that making the hulls of the Alpha Class Attack Boats out ot Titanium
was a Good Idea. "Let's see - we'll make teh hull out of something
that falls apart when there's Hydrogen around, immerse it in seawater,
and stick venting Lead/Acid Batteries aboard, and power it with a
Nuclear Reactor that, if it gets cold, has its Primary Loop Coolant
(Bismuth, IIRC) harden into solid bars in the pipes..."

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Pete Stickney
A strong conviction that something must be done is the parent of many
bad measures. -- Daniel Webster
Henry Spencer - 27 Oct 2004 04:06 GMT
>When I read 1970 documents regarding decisions and compromises for the STS
>design, it appears that aluminum was selected due to:
>
>1.) The difficulty in building & maintaining a titanium structure...
>2.) Supply and cost of titanium versus aluminum
The version I've seen is that difficulty and cost looked like a wash:
titanium was more expensive and harder to work with, but it wouldn't
require advancing the thermal-protection technology quite so far. On
purely technical issues, it looked pretty even. The decisive issue was
the USAF's fear that titanium orbiters would occupy so much of the US's
limited titanium production capacity as to interfere with F-15 production.
(The F-15 is primarily aluminum but does use significant amounts of
titanium.)

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"Think outside the box -- the box isn't our friend." | Henry Spencer
-- George Herbert | henry@spsystems.net
Pat Flannery - 27 Oct 2004 07:39 GMT
>The version I've seen is that difficulty and cost looked like a wash:
>titanium was more expensive and harder to work with, but it wouldn't
[quoted text clipped - 4 lines]
>(The F-15 is primarily aluminum but does use significant amounts of
>titanium.)
Given who made it, I'm surprised it wasn't stainless steel honeycomb,
like the B-70. ;-)
Would the use of Titanium have led to the cadmium embrittlement problems
in regards to tools used on the orbiter during maintenance, like
happened on the A-12/SR-71?
Pat
Henry Spencer - 27 Oct 2004 14:16 GMT
>>purely technical issues, it looked pretty even. The decisive issue was
>>the USAF's fear that titanium orbiters would occupy so much of the US's
>>limited titanium production capacity as to interfere with F-15 production...
>
>Given who made it, I'm surprised it wasn't stainless steel honeycomb,
>like the B-70. ;-)
That would actually be more likely if somebody else had made it.
NAA/Rockwell knew better, after all the grief they had on the B-70!
>Would the use of Titanium have led to the cadmium embrittlement problems
>in regards to tools used on the orbiter during maintenance, like
>happened on the A-12/SR-71?
Most likely, yes -- they'd have run into all the same problems as the
Blackbirds, although they might have been able to get Kelly Johnson's boys
to give them a few lectures on the basics. :-)
(And to think that Johnson used titanium because one look at the complex
manufacturing of the B-70's stainless-steel honeycomb scared him...)

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"Think outside the box -- the box isn't our friend." | Henry Spencer
-- George Herbert | henry@spsystems.net