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Aerospace Grade Nomex® Honeycomb

 

AHN4120 ARAMID FIBER/PHENOLIC COATED HONEYCOMB

 

AHN 4120 is an Aerospace Grade Nomex® Honeycomb which exhibits high strength and toughness in a small cell, low density, non-metallic honeycomb.

 

It is particularly noted for its corrosion resistance. This material is fire resistant and is typically used in transport aircraft construction where low O.S.U., smoke, and toxicity characteristics are a necessity.

 

This material also exhibits good thermal insulation properties and also has good dialectic properties. This honeycomb is easily machined, formed, and shaped and well suited to adhesive bonding.

 

PRODUCT DESIGNATION

A wide variety of cell sizes, web gauges, resin coating weights, and cell shapes are available. Strength characteristics are illustrated below. The products are designated as follows:

AHNAdvanced Honeycomb Nomex®
4120Aerospace Grade
1/8Cell size in inches
3.0Density in pounds per cubic foot
(2.0)Thickness of Aramid (in millimeters)
(for curved surfaces, if omitted the cell shape is hexagonal)
OXIndicates Over-Expanded Cell shape
(for curved surfaces, if omitted the cell shape is hexagonal)

SPECIFICATIONS
AHN 4120 honeycomb meets most commercial specifications. These include the strength requirements of BMS 8-124, DMS 1974, AMS 3711, and MIL-C-81986. Because of the large number of specifications and frequent revisions, we must be advised as to your requirements when we quote. If no specification is stated, we will certify to our Product Data sheet.

 

AVAILABILITY
AHN 4120 is supplied in standard sheet sizes of 48”L by 96”W for hexagonal shaped cells and 38”L by 96”W for over-expanded shaped cells. The sheet thicknesses can be custom cut from .060 inches up depending on customer’s requirement, material cell size and density.

 

Special sheet sizes, both larger and smaller are available on a special order basis. Because of the special size, a minimum order may be required.

 

SHEET SIZE TOLERANCES
Length (W) & Width (L) = -0 +4 inches
Thickness (T) = +/- .006 up to 2.00 inches
= .010 to 4.00 inches
= .060 above 4.00 inches

Closer tolerances are possible and may carry a premium price.

 

PRODUCT
Compressive Strength
Plate Shear
DESIGNATION
Bare
Stabilized
L Direction
W Direction
Cell Density
Strength PSI
Strength PSI
Strength PSI
Modulus ksi
Strength PSI
Modulus ksi
Hexagonal Cell
typ
min
typ
min
typ
min
typ
typ
min
typ
AHN-4120-1/8-1.8105701158090663.850361.8
AHN-4120-1/8-3.03001803252701751625.2100852.5
AHN-4120-1/8-4.05203305754702552257.01401123.6
AHN-4120-1/8-5.07006007706603252508.51751404.6
AHN-4120-1/8-6.01050800112582538526010.02001354.7
AHN-4120-1/8-8.0167511001830125046040013.02602006.5
AHN-4120-1/8-9.0200014002100160051542515.03002408.0
AHN-4120-3/16-1.590751008575603.040321.6
AHN-4120-3/16-2.014590160105110724.360402.0
AHN-4120-3/16-3.03001803252701751404.5100672.5
AHN-4120-3/16-4.04003205404702452257.01401123.8
AHN-4120-3/16-6.0700580102065042036013.02252004.5
AHN-4120-1/4-1.58045905470451.835231.3
AHN-4120-1/4-2.014080155105105722.250381.8
AHN-4120-1/4-3.02001602502251701274.580642.5
AHN-4120-1/4-3.12851803102401851355.690753.0
AHN-4120-1/4-4.04403104803602502006.5125953.5
AHN-4120-1/4-4.8n/a320n/a450n/a2257.3n/a1404.0
AHN-4120-3/8-1.585451055570451.835231.0
AHN-4120-3/8-2.01408015510590722.255361.3
AHN-4120-3/8-3.02901753202101851103.995552.5
Over-Expanded Cell
AHN-4120-3/16-1.8 OX110701207565451.560422.2
AHN-4120-3/16-3.0 OX320230350280115902.2135904.5
AHN-4120-3/16-4.0 OX6005006505501301154.31501308.0
Aircraft Flooring Core
AHN-4120-AFC-5.07005507456003552758.52051504.5
AHN-4120-AFC-9.0180014002050160048042515.03202758.0

All tests are per MIL–STD–401B, core thickness of .500″ (for core (T) of .270 increase shear strengths by 14%). Min indicates a specification minimum value. Typ indicates averages of typical production test results, actual results may be lower.

 

2024 Axiom Materials, Inc

Axiom Materials, Inc believes that the technical data and other information provided herein was materially accurate as of the date this document was issued. We reserve the right to update, revise or modify such technical data and information at any time.

 

The above is made in lieu of all warranties, expressed, or implied: Seller’s only obligation shall be to replace such quantity of this product which has proven to not substantially comply with the data presented in this bulletin. In the event of discovery of a non-conforming product, Seller shall not be liable for any commercial loss or damage, direct or consequential, arising out of the use of the inability to use the product. Before using, Buyer shall determine the suitability of the product for their intended purpose, and Buyer assumes all risk and liability whatsoever in connection therein. Statements relating to possible use of our product are not guarantees that such use is free of patent infringement or that they are approved for such use by any agency.

Applicable Markets

Aerospace

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