Core Material, Aluminum, for Sandwich Construction
- Aerospace Material Specification
- AMSC7438A
- Reaffirmed
Scope
Rationale
Recommended Content
Aerospace Standard | RIVET, UNIVERSAL HEAD, HIGH TEMPREATURE, 347 CRES UNS S34700 |
Aerospace Material Specification | Sealing Compound, Fuel-Resistant, Integral Fuel Tanks and Fuel Cell Cavities |
Aerospace Material Specification | Aluminum Foil for Sandwich Construction |
Topic
Data Sets - Support Documents
Title | Description | Download |
---|---|---|
Unnamed Dataset 1 | ||
Unnamed Dataset 2 | ||
Unnamed Dataset 3 | ||
Unnamed Dataset 4 | ||
Unnamed Dataset 5 | ||
Unnamed Dataset 6 | ||
TABLE 1 | PHYSICAL PROPERTY REQUIREMENTS. | |
TABLE 2 | ALUMINUM CORE FOIL THICKNESS, INCH. | |
TABLE 3 | TABLES OF COMPRESSIVE AND SHEAR STRENGTH REQUIREMENTS | |
TABLE 4 | MECHANICAL PROPERTIES OF 5052 ALUMINUM HONEYCOMB CORE AT ROOM TEMPERATURE (70 TO 85 °F). | |
TABLE 5 | MECHANICAL PROPERTIES OF 5052 ALUMINUM HONEYCOMB CORE AT 350 °F ± 10. | |
TABLE 6 | MECHANICAL PROPERTIES OF 5056 ALUMINUM HONEYCOMB CORE AT ROOM TEMPERATURE (70 TO 85 °F). | |
TABLE 7 | MECHANICAL PROPERTIES OF 5056 ALUMINUM HONEYCOMB CORE AT 350 °F ± 5. | |
TABLE 8 | DELAMINATION STRENGTH OF 5052 AND 5056 ALUMINUM CORE MATERIAL (GRADE B) IN POUNDS LOAD (FORCE) | |
TABLE 9 | VISUAL IMPERFECTIONS (MAXIMUM NUMBER IN A SQUARE FOOT OF MATERIAL) | |
TABLE 10 | QUALITY CONFORMANCE TESTING | |
TABLE 11 | FIRST ARTICLE TESTING |
Issuing Committee
AMS P17 Polymer Matrix Composites Committee
AMS P-17, Polymer Matrix Composites, is a technical committee in SAE’s Aerospace Materials Systems Group with the responsibility to develop and maintain material specifications and other SAE technical reports for composite materials, including prepregs, reinforcing fibers and fabrics, matrix resins, adhesives, and core materials. The committee works in conjunction with related bodies such as the Composite Materials Handbook -17 (CMH-17), ASTM Committee D30 on Composite Materials, the National Center for Advanced Materials Performance (NCAMP), the Performance Review Institute (PRI), and regulatory authorities such as FAA and EASA.
Reference
Number | Title |
---|---|
A-A-203 | This document is not part of the subscrption. |
AMSA81596 | Aluminum Foil for Sandwich Construction |
AMSQQA250/4 | ALUMINUM ALLOY 2024, PLATE AND SHEET |
AMSQQA250/5 | ALUMINUM ALLOY ALCLAD 2024, PLATE AND SHEET |
AMSSTD401 | Sandwich Constructions and Core Materials; General Test Methods |
ANSI/ASQ Z1.4 | This document is not part of the subscrption. |
ASTMB117 | This document is not part of the subscrption. |
ASTMC366 | This document is not part of the subscrption. |
ASTMD1974 | This document is not part of the subscrption. |
ASTMD3951 | This document is not part of the subscrption. |
ASTMD5118 | This document is not part of the subscrption. |
ASTMD5168 | This document is not part of the subscrption. |
ASTMD6251 | This document is not part of the subscrption. |
MIL-DTL-17667 | This document is not part of the subscrption. |
MIL-STD-2073-1 | This document is not part of the subscrption. |