MIL-S-25392 Revision B:1968
Current
The latest, up-to-date edition.
Sandwich Construction, Plastic Resin, Glass Fabric Base, Laminated Facings and Polyurethane Foamed-in-Place Core, For Aircraft Structural Applications
08-05-1968
Important note : Users cannot be edited or removed once added to your Multi user PDF.Details the above plastic molded construction for aircraft structural applications up to 350 deg. F, including aircraft external plastic parts, and other weapons applications.
| DevelopmentNote |
INACTIVE FOR NEW DESIGN 31/7/96
|
| DocumentType |
Standard
|
| Pages |
16
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Current
|
This specification covers plastic molded sandwich construction using glass fabric base plastic laminate facings and urethane foamed-in-place core material for aircraft structural and applications up to 350 degrees F, including all aircraft external plastic parts, and other weapons applications.
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