4 ms·

You have way more insight than I do. What you describe reminds me of a complicated webbing of aluminum to hold everything in place. If I understand you correctl

by jfoutz 12y ago

You have way more insight than I do. What you describe reminds me of a complicated webbing of aluminum to hold everything in place. If I understand you correctly having access to a titanium equivalent could do two things. One, you could reduce part count, replace an array of aluminum supports with one titanium part. If the strength and weight are about the same, the simpler design seems better to me. Two, you could free up some space for other stuff. I'm thinking fuel tanks in wings, but i'm not even at the level of armchair aerospace engineer. There are probably many cases where aluminum is lighter but bulkier. Opening up a channel to simplify wiring, or hydraulics could be helpful.

damoncali 12y ago
The trouble is that it's not a lot of space, and it's not as simple as stiffness/weight of the material. Think about something simple like a structural tube. The diameter of the tube has significantly more impact on it's stiffness than it's material. So if you use a 30% lighter, but strong enough material, you can add 30% to the cross sectional area of the tube- which means you can make it a bit bigger in diameter, which will have potentially huge impacts on overall structural stiffness. Note that adding 30% more material will add at least 30% more strength to the part (huge oversimplification here, but just for arguments sake, we'll use that simple tensile case). Titanium was useful when we needed very high strength on a very large part - a good example is the trunnions that attach payloads to the space shuttle cargo bay. These are large metal bars a little over 3 inches in diameter and maybe a couple feet in length. Aluminum is not strong enough. Steel would be punishingly heavy. (do the math - these things are beasts). So titanium can be a good fit for stuff like that. But most steel parts were small - things like bolts, rod ends an the like. They tend to be specialized with very specific detailed requirements for things like fatigue, frictional characteristics, and that sort of thing. Because they are small, the weight just isn't that big an issue. Bigger stuff was almost always aluminum, which is actually a lot stronger than most folks realize. At least, the good stuff is. Titanium also has some other odd properties that make it troublesome in space. I wasn't a materials guy, but they were always bitching about "hydrogen embrittlement" and the fact that large titanium parts do not burn up on re-entry like aluminum does, which presents a debris hazard to people on the ground. (I don't know how big a problem that really is, but people didn't want to be dumping space junk on top of people's heads. Honestly, I just took this on faith - people were concerned about it, but it always struck me as odd.)
- dsjoerg 12y ago
  If I had a nickel for each time I heard a guy bitching about "hydrogen embrittlement", I'd fund this space program myself!
- Demiurge 12y ago
  By 'aluminum' do you mean 'duralumin' or just aluminum? My uncle had a few tiles of duralumin in garage, and I remember it was definitely a lot harder than plain aluminum.
  - damoncali 12y ago
    Almost everything we used was plain old 6061 aluminum - the "standard" alloy everyone uses for everything. If a little more strength was needed, 7075 would usually do the trick.
    - WildUtah 12y ago
      Funny that I've started to think of Apple's easily CNC'd aluminium as the standard instead of 6061. That Apple stuff is about as strong as wax, not even as tough as others' plastic shells. Sure looks good on my iPhone and MacBook, though. I'm glad to have 6061 on my bike instead.
- jfoutz 12y ago
  Oh, i think i get it. The materials are different, but not different enough for a whole different design - you can't generally simplify out parts. Some strut being 1cm across vs 1.2 cm across doesn't buy you much. Thanks!
  - darkmighty 12y ago
    To better understand the comment above you need to understand stiffness. When you take a wire of steel, which is very strong, you'll find you can actually bend it very easily. If this kind of stress is what the material will face, you could replace the wire by a thin tube which will be much more rigid -- you probably don't want your structure bending and deforming. In this case, where stiffness is more important, it's more important that the material is light so you can make it larger yet proportionally stiffer per unit weight by using an adequate structure -- e.g. a tube or large diameter (this is because the bending stiffness increases more-than-linearly with diameter). Now suppose instead you were trying to traction the wire (pull it). There's no structural change that will make it stiffer -- in this case all you may want is that it is very strong -- in which case you simply go for the best strength/weight or just pure strength.

by jfoutz 12y ago

damoncali 12y ago

The trouble is that it's not a lot of space, and it's not as simple as stiffness/weight of the material. Think about something simple like a structural tube. The diameter of the tube has significantly more impact on it's stiffness than it's material. So if you use a 30% lighter, but strong enough material, you can add 30% to the cross sectional area of the tube- which means you can make it a bit bigger in diameter, which will have potentially huge impacts on overall structural stiffness. Note that adding 30% more material will add at least 30% more strength to the part (huge oversimplification here, but just for arguments sake, we'll use that simple tensile case). Titanium was useful when we needed very high strength on a very large part - a good example is the trunnions that attach payloads to the space shuttle cargo bay. These are large metal bars a little over 3 inches in diameter and maybe a couple feet in length. Aluminum is not strong enough. Steel would be punishingly heavy. (do the math - these things are beasts). So titanium can be a good fit for stuff like that. But most steel parts were small - things like bolts, rod ends an the like. They tend to be specialized with very specific detailed requirements for things like fatigue, frictional characteristics, and that sort of thing. Because they are small, the weight just isn't that big an issue. Bigger stuff was almost always aluminum, which is actually a lot stronger than most folks realize. At least, the good stuff is. Titanium also has some other odd properties that make it troublesome in space. I wasn't a materials guy, but they were always bitching about "hydrogen embrittlement" and the fact that large titanium parts do not burn up on re-entry like aluminum does, which presents a debris hazard to people on the ground. (I don't know how big a problem that really is, but people didn't want to be dumping space junk on top of people's heads. Honestly, I just took this on faith - people were concerned about it, but it always struck me as odd.)

dsjoerg 12y ago
If I had a nickel for each time I heard a guy bitching about "hydrogen embrittlement", I'd fund this space program myself!
Demiurge 12y ago
By 'aluminum' do you mean 'duralumin' or just aluminum? My uncle had a few tiles of duralumin in garage, and I remember it was definitely a lot harder than plain aluminum.
- damoncali 12y ago
  Almost everything we used was plain old 6061 aluminum - the "standard" alloy everyone uses for everything. If a little more strength was needed, 7075 would usually do the trick.
  - WildUtah 12y ago
    Funny that I've started to think of Apple's easily CNC'd aluminium as the standard instead of 6061. That Apple stuff is about as strong as wax, not even as tough as others' plastic shells. Sure looks good on my iPhone and MacBook, though. I'm glad to have 6061 on my bike instead.
jfoutz 12y ago
Oh, i think i get it. The materials are different, but not different enough for a whole different design - you can't generally simplify out parts. Some strut being 1cm across vs 1.2 cm across doesn't buy you much. Thanks!
- darkmighty 12y ago
  To better understand the comment above you need to understand stiffness. When you take a wire of steel, which is very strong, you'll find you can actually bend it very easily. If this kind of stress is what the material will face, you could replace the wire by a thin tube which will be much more rigid -- you probably don't want your structure bending and deforming. In this case, where stiffness is more important, it's more important that the material is light so you can make it larger yet proportionally stiffer per unit weight by using an adequate structure -- e.g. a tube or large diameter (this is because the bending stiffness increases more-than-linearly with diameter). Now suppose instead you were trying to traction the wire (pull it). There's no structural change that will make it stiffer -- in this case all you may want is that it is very strong -- in which case you simply go for the best strength/weight or just pure strength.