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Glass, Monolithic, Aircraft Glazing
- Aerospace Material Specification
Published June 29, 2016 by SAE International in United States
Downloadable datasets availableAnnotation ability available
This specification covers monolithic glass for use in aircraft glazing. (see 6.1.)
This document has been determined to contain basic and stable technology which is not dynamic in nature.
|Aerospace Standard||CONTACTS, ELECTRICAL CONNECTORS, SOCKET, SOLDER, REMOVABLE, SHIELDED, SIZE 12 (FOR MIL-DTL-83723 SERIES III AND MIL-DTL-83527 CONNECTORS)|
|Aerospace Material Specification||Insulation, Electrical, Pasted-Mica|
|Aerospace Material Specification||Titanium Alloy Bars, Forgings and Forging Stock 8Al - 1Mo - 1V Duplex Annealed|
Data Sets - Support Documents
|[Unnamed Dataset 1]|
|[Unnamed Dataset 2]|
|TABLE I||Nominal thickness and tolerance in thickness and dimensions of annealed glass|
|TABLE II||Original luminous transmittance|
|TABLE III||Solar-radiation transmittance for type III glass|
|TABLE IV||Allowable minor defects|
|[Unnamed Dataset 7]||Identification from (example)|
|TABLE V||Normal incidence deviation data|
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