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MIL-PRF-32568_NOT_1-003 (1).pdf
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Comments, suggestions, or questions on this document should be addressed to: Commander, Naval Sea Systems
Command, ATTN: SEA 05S, 1333 Isaac Hull Avenue, SE, Stop 5160, Washington Navy Yard DC 20376-5160 or
emailed to CommandStandards@navy.mil, with the subject line “Document Comment”. Since contact information
can change, you may want to verify the currency of this address information using the ASSIST Online database at
https://assist.dla.mil.
AMSC N/A FSC 7210
DISTRIBUTION STATEMENT A. Approved for public release. Distribution is unlimited.
INCH-POUND
MIL-PRF-32568
20 December 2016
PERFORMANCE SPECIFICATION
MATTRESS, INNERSPRING, FLAME RESISTANT, SHIPBOARD
This specification is approved for use by all Departments and Agencies of the Department of Defense.
1. SCOPE
1.1 Scope. This specification covers flame resistant innerspring shipboard mattresses (see 6.3.5) for use aboard
U.S. Navy vessels.
1.2 Classification. The mattresses covered by this specification are of the following sizes, as specified
(see 6.2).
1.2.1 Sizes. The sizes of mattress are as follows (see 3.5):
a. 1 – Crew (Short)
b. 2 – Crew (Regular)
c. 3 – Crew (Long)
d. 4 – Chief Petty Officer (CPO) (Regular)/Officer (Narrow)
e. 5 – CPO (Long)
f. 6 – Crew Sub (Small)
g. 7 – Crew Sub (Regular)
h. 8 – Officer (Wide)
i. 9 – Officer/CPO Sub
Source: https://assist.dla.mil -- Downloaded: 2023-02-13T20:06Z
Check the source to verify that this is the current version before use.
MIL-PRF-32568
2
1.3 Part or identifying number (PIN). PINs to be used for a mattress acquired to this specification are created
as follows:
M
32568
-
X
Prefix for Military
Specification
Specification
Number
-
Size (see
code below)
Size Code
Size
Code
1
1
2
2
3
3
4
4
5
5
6
6
7
7
8
8
9
9
Examples:
M32568-1
M32568-8
2. APPLICABLE DOCUMENTS
2.1 General. The documents listed in this section are specified in sections 3 or 4 of this specification. This
section does not include documents cited in other sections of this specification or recommended for additional
information or as examples. While every effort has been made to ensure the completeness of this list, document
users are cautioned that they must meet all specified requirements of documents cited in sections 3 or 4 of this
specification, whether or not they are listed.
2.2 Government documents.
2.2.1 Specifications, standards, and handbooks. The following specifications, standards, and handbooks form a
part of this document to the extent specified herein. Unless otherwise specified, the issues of these documents are
those cited in the solicitation or contract.
COMMERCIAL ITEM DESCRIPTIONS
A-A-50195
-
Thread, Aramid
DEPARTMENT OF DEFENSE STANDARDS
MIL-STD-129
-
Military Marking for Shipment and Storage
(Copies of these documents are available online at http://quicksearch.dla.mil.)
2.2.2 Other Government documents, drawings, and publications. The following other Government documents,
drawings, and publications form a part of this document to the extent specified herein. Unless otherwise specified,
the issues of these documents are those cited in the solicitation or contract.
Source: https://assist.dla.mil -- Downloaded: 2023-02-13T20:06Z
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MIL-PRF-32568
3
NAVAL SEA SYSTEMS COMMAND (NAVSEA) PUBLICATIONS
S9510-AB-ATM-010
-
Nuclear Powered Submarine Atmosphere Control Manual
(Copies of the chapter titled “Material Control Program” are available by email request to
CommandStandards@navy.mil.)
2.3 Non-Government publications. The following documents form a part of this document to the extent
specified herein. Unless otherwise specified, the issues of these documents are those cited in the solicitation or
contract.
ASTM INTERNATIONAL
ASTM D1424
-
Standard Test Method for Tearing Strength of Fabrics by Falling-
Pendulum (Elmendorf-Type) Apparatus
ASTM D3574
-
Standard Test Methods for Flexible Cellular Materials – Slab,
Bonded, and Molded Urethane Foams
ASTM D3776/D3776M
-
Standard Test Method for Mass Per Unit Area (Weight) of Fabric
ASTM D5034
-
Standard Test Method for Breaking Strength and Elongation of
Textile Fabrics (Grab Test)
ASTM D6193
-
Standard Practice for Stitches and Seams
ASTM D6413/D6413M
-
Standard Test Method for Flame Resistance of Textiles (Vertical
Test)
ASTM D6988
-
Standard Guide for Determination of Thickness of Plastic Film Test
Specimens
ASTM E162
-
Standard Test Method for Surface Flammability of Materials Using a
Radiant Heat Energy Source
ASTM E662
-
Standard Test Method for Specific Optical Density of Smoke
Generated by Solid Materials
ASTM E800
-
Standard Guide for Measurement of Gases Present or Generated
During Fires
ASTM E1590
-
Standard Test Method for Fire Testing of Mattresses
ASTM F1566
-
Standard Test Methods for Evaluation of Innersprings, Boxsprings,
Mattresses or Mattress Sets
(Copies of these documents are available online at www.astm.org.)
INTERNATIONAL ORGANIZATION FOR STANDARDIZATION (ISO)
ISO/IEC 17025
-
General Requirements for the Competence of Testing and Calibration
Laboratories
(Copies of this document are available online at www.iso.org.)
2.4 Order of precedence. Unless otherwise noted herein or in the contract, in the event of a conflict between
the text of this document and the references cited herein, the text of this document takes precedence. Nothing in this
document, however, supersedes applicable laws and regulations unless a specific exemption has been obtained.
Source: https://assist.dla.mil -- Downloaded: 2023-02-13T20:06Z
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MIL-PRF-32568
4
3. REQUIREMENTS
3.1 First article. When specified (see 6.2), a sample shall be subjected to first article inspection in accordance
with 4.1.
3.2 Components. All component materials of the mattress shall be flame resistant and conform to the
requirements of table I.
3.2.1 Recycled, recovered, environmentally preferable, or biobased materials. Recycled, recovered,
environmentally preferable, or biobased materials should be used to the maximum extent possible, provided that the
material meets or exceeds the operational and maintenance requirements, and promotes economically advantageous
life cycle costs.
TABLE I. Component requirements.
Component
Characteristic
Requirement
Border ticking, upholstery
ticking
Tear strength
Warp: 3.5 lbs min.; Filling: 3.5 lbs min.
Breaking strength
Warp: 94 lbs min.; Filling: 58 lbs min.
Weight (oz/yd²)
6.5 (min.); 8.5 (max.)
Insulator fabric
Tear strength
Warp: 4.0 lbs min.; Filling: 1.5 lbs min.
Breaking strength
Warp: 70 lbs min.; Filling: 20 lbs min.
Upholstery ticking
1/
, border
ticking
1/
, insulator fabric,
flange, and tape
2/
Flammability:
Char length
5.0 inches max.
After flame
2.0 seconds max.
Molten or flaming drops
None
Cushioning pad and quilting
foam
Flammability:
Flame spread
10 (max.) and no molten or flaming drops
Smoke density, D
MAX
200 and no molten or flaming drops
2/
Fire gas toxicity
3/
NOTES:
1/
The flammability tests shall be performed in the initial condition and after conducting 15
laundering cycles (see table IV).
2/
The only characteristic the tape is required to meet is the molten or flaming drops requirement.
3/
See 3.8.2.
3.2.2 Ticking fabric. The ticking (see 6.3.10) fabric shall be permanently fire retardant and have an alternating
blue warp stripe pattern on bleached or natural white background. The flammability and physical requirements shall
be as required by table I.
3.2.3 Thread. The thread used for assembling components of the mattress shall be polyaramid in accordance
with A-A-50195 in size, finish, and ply to meet all requirements of this specification. Nylon thread shall be used for
quilting of sleeping surfaces to ensure that the mattress will meet durability requirements.
Source: https://assist.dla.mil -- Downloaded: 2023-02-13T20:06Z
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MIL-PRF-32568
5
3.2.4 Innerspring core. The innerspring core (see 6.3.2) shall be constructed from 14.5-gauge all-wire carbon
steel to ensure that the firmness and durability requirements are met. The coils shall be assembled and fixed into
individual rows to suit the length and width of the mattress size specified. The core shall be designed to extend to
the full length and width of the finished mattress (see table III). The tolerance for the core when inside a finished
mattress shall not recede more than ½ inch in the length direction on each side and no more than ¼ inch in the width
direction on each side when measured from the mattress stitch line. The coils shall be permanently secured to
provide long-term structural stability. The coils shall be assembled into a spring core unit by helically linking the
individual coils.
3.2.5 Quilting foam. The quilting foam shall consist of flame resistant cushioning upholstery (see 6.3.11) foam
that is integral with a fabric scrim backing.
3.2.5.1 Quilting foam density. The density of quilting foam shall be 6.0±1.0 pounds per cubic foot (lb/ft³)
when tested in accordance with 4.5.1.b.
3.2.5.2 Quilting foam compression set. The compression set of the quilting foam shall be 12 percent maximum
at a 50 percent deflection when tested in accordance with 4.5.1.d.
3.2.5.3 Quilting foam tensile strength. The tensile strength of the quilting foam shall be 5.0 pounds per square
inch (lb/in
2
) minimum when tested in accordance with 4.5.1.e.
3.2.5.4 Quilting foam flammability. The quilting foam flammability shall be in accordance with the
requirements in table I when tested in accordance with table IV.
3.2.6 Insulator fabric. The insulator fabric shall be 100 percent cotton, plain weave to ensure a durable layer is
provided to protect the foam cushioning pad from spring coils and to ensure fabric will not melt or drip when
exposed to elevated temperatures. The weight shall be 3.6±0.3 ounces per square yard (oz/yd
2
), and have a
minimum thread count of 30 in the warp direction and 25 in the fill direction. The fire performance shall be as
required by table I when tested in accordance with table IV.
3.2.7 Cushioning pad (topper). The cushioning pad (see 6.3.3) shall be flame resistant synthetic foam.
3.2.7.1 Cushioning pad thickness. The thickness of the cushioning pad shall be no less than ½±
1
⁄
16
inch thick
and shall be determined in accordance with 4.5.1.a.
3.2.7.2 Cushioning pad density. The density of the cushioning pad shall be 7.2±0.7 lb/ft³ when tested in
accordance with 4.5.1.b.
3.2.7.3 Cushioning foam indentation force deflection (IFD). The cushioning foam shall have an IFD of
47±7 pounds at 25 percent deflection at a 2-inch thickness when tested in accordance with 4.5.1.c.
3.2.7.4 Cushioning pad compression set. The compression set of the cushioning pad shall be 10 percent
maximum for a 50 percent deflection when tested in accordance with 4.5.1.d.
3.2.7.5 Cushioning pad tensile strength. The tensile strength of the cushioning pad shall be 12 lb/in² minimum
when tested in accordance with 4.5.1.e.
3.2.7.6 Cushioning pad tear strength. The tear strength of the cushioning pad shall be 2.5 lb/in minimum when
tested in accordance with 4.5.1.f.
3.2.7.7 Cushioning pad resiliency. The resiliency of the cushioning pad shall be 30 percent minimum when
tested in accordance with 4.5.1.g.
3.2.7.8 Cushioning pad dry heat aging. The change in IFD after dry heat aging shall be 20 percent maximum
when tested in accordance with 4.5.1.h.
3.2.7.9 Cushioning pad foam flammability. The cushioning pad foam flammability shall be in accordance with
the requirements in table I when tested in accordance with table IV.
Source: https://assist.dla.mil -- Downloaded: 2023-02-13T20:06Z
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