
www.Usenet.com
| <-- __Chronological__ --> | <-- __Thread__ --> |
"Josh Halpern" <[EMAIL PROTECTED]> wrote in message news:[EMAIL PROTECTED] > Grant Kiehne wrote: > >Does anyone have experience using anodized aluminum parts in a high > >vacuum or ultra-high vacuumm (UHV) system? I am investigating using > >some relatively large-area anodized aluminum parts in a system that > >must achieve ~5x10^-8 Torr (cool) after baking at 135 deg. C for ~12 > >hrs. The alloys are 6061-T4 and 6063-T5. This yields a > >fresh native oxide on the aluminum surface. My application requires a > >thicker oxide layer (microns). > >Grant > > > Generally one uses stainless steel for high vacuum. > Al might be ok for 10-8 > josh halpern > Yo, Josh, old bud, Easy on the that "generally". I think that all non-load bearing, non-ablating space vehicle skins are made from Aluminum, 2024, 6061 or 7075, about the thickness of a beer can. Most of it is not even anodized, but bare, maybe CrO4/SiF6 treated. The pressure in space at 130 - 140 miles up is about 10e-6 torr. 250 miles up at MIR we have a vacuum of about 10e-8 torr, and at the Hubble Space Telescope at about 370 miles up the pressure is near 10e-9 torr. Alu appears to serve quite well. Have fun, Josh, hanson
| <-- __Chronological__ --> | <-- __Thread__ --> |