Zerodur
From Wikipedia, the free encyclopedia
Zerodur®, a registered trademark of Schott Glass Technologies,[1] is a lithium aluminosilicate glass-ceramic[2] produced by Schott AG since 1968.[3] It has been used for a number of very large telescope mirrors including Keck I and Keck II.[4] With its very low coefficient of expansion it can be used to produce mirrors which retain acceptable figures in extremely cold environments such as deep space.[5] Although it has advantages for applications requiring COE less than that of borosilicate glass it remains very expensive as compared to borosilicate.
Zerodur has both an amorphous (vitreous) component and a crystalline component. Its most important properties[6] are:
- Low thermal expansion (≈0.2 × 10−7/K at 0 °C–50 °C) which is an order of magnitude better than that of fused quartz
- High 3D homogeneity with few inclusions, bubbles and internal stria - (as contrasted to Cer-Vit)
- Hardness similar to borosilicate glass so that it can be ground and polished more easily than fused quartz
- High affinity for coatings
- Low helium permeability
- Non-porous - (as contrasted to sintered ceramics)
- Good chemical stability similar to that of fused quartz
- Fracture toughness approximately 0.9 MPa x m1/2 [2]
Contents |
[edit] Applications
The Keck II Telescope showing the segmented primary mirror made of Zerodur
- Optics
- Microlithography
- Measurement technology[3]
[edit] Properties[6]
- Dispersion: (nf − nc) = 0.00967
- Density: 2.53 g/cm3 at 25 °C
- Young's Modulus: 9.1 x 1010 Pa
- Poisson Ratio: 0.24
- Specific heat capacity at 25 °C: 0.196 cal/(g·K) = 0.82 J/(g·K)
- Coefficient of thermal expansion (20 °C to 300 °C) : 0.05 ± 0.10 × 10−6/K
- Thermal conductivity: at 20 °C: 1.46 W/(m·K)
- Maximum temperature: 600 °C
- Impact resistance behavior is substantially similar to other glass[7]
[edit] See also
[edit] References
- ^ http://www.unitedlens.com/page175.html
- ^ a b Viens, Michael J (April 1990). "Fracture Toughness and Crack Growth of Zerodur" (PDF). NASA Technical Memorandum 4185. NASA. http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19900011871_1990011871.pdf. Retrieved 28 August 2011.
- ^ a b Schott AG Zerodur description
- ^ Döhring, Thorsten; Peter Hartmann, Ralf Jedamzik, Armin Thomas, Frank-Thomas Lentes. "Properties of Zerodur Mirror Blanks for Extremely Large Telescopes" (PDF). Proc. of SPIE Vol. 6148 61480G-8. SPIE. http://www.optics.arizona.edu/optomech/Fall10/grad%20student%20reports/Properties%20of%20Zerodur%20Mirrors%20for%20Large%20Telescopes.pdf. Retrieved 26 August 2011.
- ^ Baer, JW; WP Lotz. "Figure testing of 300 mm Zerodur mirrors at cryogenic temperatures" (PDF). http://www.4dtechnology.com/reflib/Figure%20testing%20of%20300%20mm%20Zerodur%20mirrors%20at%20cryogenic%20temper.pdf. Retrieved 26 August 2011.
- ^ a b Schott AG Zerodur properties
- ^ Senf, H; E Strassburger, H Rothenhausler (1997). "A study of Damage during Impact in Zerodur" (in English). J Phys Iv France 7 (Colloque C3, Suppltment au Journal de Physique I11 d'aotit 1997). http://hal.archives-ouvertes.fr/docs/00/25/54/63/PDF/ajp-jp4199707C3171.pdf. Retrieved 31 August 2011.
[edit] External links
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