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
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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