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Composite Panels - H8PP 18oz WR
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Due to anisotropic properties of honeycombs, MIL handbook 17B does not recommend ASTM C393, or 3 point bend test as a valid indicator of honeycomb cored panel behavior. It is viewed as a possible quality control test but not indicative of the real attributes of the structure. It is generally felt that a better indicator would be the ASTM D 6146-99) (Standard Test Method for Two-dimensional Flexural Properties of Simply Supported Sandwich Composite Plates Subjected to a Distributed Load) or also known as "The Hydramat test". These tests have produced results that validate the accompanying Strength of Materials Data. The viscoelastic behavior of Nida-Core Polypropylene Honeycomb will typically permit far greater deflections without structural failures so the Deflection at Load is supplied for comparison but this does not imply a Load to fail.

All tests carried out by independent laboratory. This information is provided in good faith and is subject to modifications without prior notification. It does not constitute a commitment, neither a contractual document. Nida-Core Corp will not assume any liability form use or misuse of data presented herein.

Assessment of suitability is the responsibility of end user only.

MATERIAL

Total

Thickness

of sandwich

inches

Modulus

(MSI)

Max Ply

Stress

(PSI)

% of each ply's ultimate strength

Bending Stiffness

Lb/sq.inch

Total weight

Lb/ft2

Flatwise compression

Fmax/

Area

(PSI)

Nida-Core H8PP 10 mm + 18 oz WR both sides

0.448

1.95

0

1.95

42000

0

42000

100

0

100

4972

0.662

188

Nida-Core H8PP 13 mm + 18 oz WR both sides

0.568

2.25

0

2.0

26300

0

26142

100

0

88.27

8929

0.712

188

Nida-Core H8PP 20 mm + 18 oz WR both sides

0.808

2.25

0

2.0

26300

0

26189

100

0

88.18

18642

0.812

188

Nida-Core H8PP 25 mm + 18 oz WR both sides

1.058

2.25

2.3

2

26300

20727

26215

100

0

88.27

32521

0.917

188

Deflection values based on 200lb point load centrally with simple support for 18 oz WR panels with H8PP core.

 

DEFLECTION

VALUES

SPAN

SPAN

SPAN

Core thickness

MM

24"

36"

48"

10

0.12"

0.27"

0.48"

13

0.067"

0.15"

0.27"

20

0.032"

0.072"

0.13"

25

0.018"

0.04"

0.073"

38

0.008"

0.018"

0.033"

50

0.005"

0.011"

0.019"

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Online Ordering
(Contact Sales Representative For Volume Discounts)

SKIN: WET-LAMINATED GLASS 18 OZ

Item # Thickness
(mm)
Thickness
(in)
Sheets/skid Price/sheet
Panel-Composite-5mm 5 0.2 100 $166.32
Quantity:
Panel-Composite-7mm 7 0.28 100 $173.97
Quantity:
Panel-Composite-10mm 10 0.38 100 $184.10
Quantity:
Panel-Composite-13mm 13 0.51 90 $193.85
Quantity:
Panel-Composite-16mm 16 0.63 80 $206.06
Quantity:
Panel-Composite-20mm 20 0.79 75 $218.14
Quantity:
Panel-Composite-25mm 25 0.98 60 $238.96
Quantity:
Panel-Composite-30mm 30 1.18 50 $260.83
Quantity:
Panel-Composite-38mm 38 1.5 40 $286.52
Quantity:
Panel-Composite-50mm 50 2 35 $329.92
Quantity:
Panel-Composite-76mm 76 3 25 $420.17
Quantity:

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Note: Sheet size = 4' x 8'.

ALUMINUM 3003 MILL FINISHED BOTH SIDES. PLEASE CALL FOR QUOTE: SANDED: ADD $ 0.15 per square foot per side
GELCOAT: Please call us. Fiberglass panels have a T102 pigment mixed in the skins. For regular Gelcoat add $.43 per SqFt. per side, for both sides $.98 SqFt.
LESS THAN A SKID: 5% ADDED TO "LESS THAN A SKID" PRICE
OTHER THICKNESSES (UP TO 18") ARE AVAILABLE BY SPECIAL ORDER.
SIZES OTHER THAN 4'X8' ARE AVAILABLE
UPON REQUEST, NIDA-CORE H8PP HONEYCOMB AND FORMICA CAN BE FLAME-RETARDANT.
NIDA-CORE OFFERS CUT-TO-SIZE CNC CAPABILITIES. PLEASE CALL FOR QUOTE.
OTHER SKINS, SUCH AS 36oz fiberglass, are available. Please call for a quote.
PLEASE CALL FOR A QUOTE CONFIRMATION. PRICES ARE SUBJECT TO CHANGE WITHOUT NOTICE.
NIDA-CORE CONDITIONS OF SALE IN THE BROCHURE AND ON THE INVOICES APPLY.
PUBLISHED QUANTITIES MUST BE STRICTLY ADHERED TO IN ORDER TO OBTAIN VOLUME DISCOUNTS. VOLUME DISCOUNTS APPLY PER PURCHASE ORDER.

PRICES ARE F.O.B. ORIGIN OR AS OTHERWISE INDICATED AND PREPAID.

NIDA-CORE LIMITS ITS WARRANTY TO THE FREE DELIVERY OF PANELS REPLACING PANELS PROVED TO BE DEFECTIVE.
NIDA-CORE EXPRESSLY DISCLAIMS ANY LIABILITY FOR CONSEQUENTIAL DAMAGES.

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