M22759/33-26-8 datasheet, PDF - EEWORLD Datasheet

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M22759/33-26-8: DescriptionWire And Cable, 1 Conductor(s), 26AWG, 600V, Flexible Cord And Fixture Wire,; CategoryThe connector Connector bracket; File Size218KB，5 Pages; ManufacturerJudd Wire

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M22759/33-26-8 Overview

Wire And Cable, 1 Conductor(s), 26AWG, 600V, Flexible Cord And Fixture Wire,

M22759/33-26-8 Parametric

Parameter Name	Attribute value
Objectid	8330094511
Reach Compliance Code	unknown
Other features	STANDARD: MIL-W-22759
Certification	MIL
Conductor surface treatment	SILVER
conductor material	COPPER ALLOY
Connector bracket type	WIRE AND CABLE
structure	STRANDED
diameter	0.81 mm
insulator material	CROSSLINKED EXTRUDED MODIFIED ETFE
Number of conductors	1
Maximum operating temperature	200 °C
Rated voltage	600 V
resistance	0.147 Ω
shield	NO
stay	19X38
Wire gauge	26 AWG
Wire and Cable Names	FLEXIBLE CORD AND FIXTURE WIRE

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141

L-N-22759133C

September 1988

MIL-i4-22759/33B

15 July 1986

MILITARY SPECIFICATION SHEET

WIRE, ELECTRICAL, FLUOROPOLYMER- INSULATCD, CR13SSLINKE0M~OIF IEO

ETFE, LIGHTUEIGHT, SILVER-COATEO. HIGH-STRENGTH cOPpER ALLOy . 200 C . 600 qoLT

This specification is approved for use by all Depart-

ments and hgencies of the Department of Oefense.

The requirements for acqui ring the wire described herein shall

consist of this.specification and the latest issue of MIL-14-22759.

SMALL 01A14ETERCOIIDUCTOR- SILVER

COATEO IIIGII STRENGTN COPPER ALLOY

“%

INSULATIOII- CROSSLINKEO,

EXTRUOEO, NOOIFIEO ETFE*

““”’.:’.

iiEiE3

,’ ETFE - Ethylene-tetrafluoroethylene,copolymer,

.,.,..

~“

F{GURE 1.

iguration.

General Con””f

,,.

TABLE 1.

Construction details.

!,,

. .. .

. . . .

I Diameter

Resistance I

Stranding

“’

Iof strandec

Part no. ~/ IiflreI

t 20”C (68”F)I Oiameter

(number of

I conductor

ohms/lDOO ft)I [inches)

[siZe [ strands x AUG I (tnches)

(ma.)

Igauge of strands)l[minlI(maxl

7x38

f1227s9/33-30-*

i 30

i.oll i.olz

7x36

H22759/33-2B-’ I 28 I

1.014 1.016

19 x 38

14227 9/33-26-’ I 26 I

1.018

1.020

M22759/33-24-* I 24 I

;; ; ;$

1.023 1.025

A422759/33-22-*I .22 I

I.029 I

.031

M22759/33-20-*

[.037 {.039

Melght

lbs/1000 ftl

(mdx)

-.66

.91

;::

2.9

4.4

Part number: The asterisks in tNe part number column, tables 1 and 11, shal1 be replaced

by color code designators in accordance with MIL-STO-681. Examples: Size 20, white -

1422759/33-20-9;white with orange stripe - N22759/33-20-93. Printing of color code designator

on surface of wire insulation is not required.

~. @

demtes changes

AMSC II(A

FSC 6145

l“of “5 “’

OISTRIRUTIOH STATEMENT .4. .4pvr0v@dfOr public release: distribution is unlimited.

Source: https://assist.dla.mil -- Downloaded: 2018-09-14T07:51Z

Check the source to verify that this is the current version before use.

MIL-w-22759/33C

F1mmnaoiIity r’e@irements and procedure:

The flammability test of MIL-N-22759 shall be modified for the

wire

of this specification sheet as

follows: The specified test burner shall be used without the wing top flame spreader and shall be

adjusted to furnis~ a 3-!nch conical f~ame with an inner cone approximately 1 inch in height and a

temperature of 955 C +30 C (1751 F *54 F) at its hottest point. A sheet of facial tissue conforming

to UU-T-450 shall be suspended taut and horizontal 9-1/2 inches .bel the marked POint On the wire

spec~rnenin the test chamber and at least 1/2 inch above

the

floor of the chamber. The period

aPPIlcatiQn Of the hot flame tip to

the

marked point on the wire specimen shal1 be 30 seconds for

all sizes of wtre. Observations shal1 fnclude time of burning after removal of the test flame,

final distance of flame travel on the wire above the test mark, and presence or absence of flame in

the facial tissue due to incendiary drip from the specimen. Requirements shall be:

Ouratfon of after-flame

Flame travel

No flaming of tissue

3 seconds (max)

3.0 inches (max)

Breaking of the wire specimen in size 24 or smali>r shall not be considered as failure provided the

requirements for duration of flame, final distance of flame travel, and absence of incendiary

dripping are met.

One specimen shal1 be tested from each sample unit. The post-flame dielectric test of MIL-!4-22759

is not required for wire of this specification sheet.

hnmersion precedure:

A 24-inch specimen, for each test fluid in table 511, shall Rave its diameter measured and shall

then be inunersedto within 6 inches of each end for ,the time and temperature specified. During

immersion, the radius of bend of the wire shall be not less than’14 nor mare than 35 times the

spacified maximum diameter of the wire under test. Upon removal fram the test fluid, the specimen

shall be wiped .dry and then remain for 1 hour in free air at room temperature. The diameter shall

be measured and compared to the initial diameter.’ The insulation shall be removed for a distance of

1/2 inch from each end of the specimen. The specimen shal1 then be subjected to the bend test and

dielectric test specified in the procedure for 1Ife cycle testing.

Propellant resistance procedure:

(Initial qualification test only)

Specimens of finished wire, 24 inches long, shill be innnersedto within 1.1/2 inches of each end in

the following propellants for the specified time at normal room temperature, using a separate

specimen for each propellant.

Propellant

MIL-P-26536, Propellant, Hydrazine

MIL.P-26539, Propellant, Nitrogen Tetroxide

MIL-P-27402, Propellant, Hydrazine - Uns-

Ofmethylhydrazine (50 percent N2H4 -

50 percent UOMH )

Inmersion time

30 minutes

1 minute

30 minutes

Ouring inznersion,the radius of bend of the wire shall be not less than 14 nor more than 35 times

the specified maximum dfameter of the wire under test. Upon removal from the 1iquids, the specimens

shal1 remain for no more than 48 hours in free air at room temperature. The insulsfon shall be

removed for a distdnce of 1 inch from each end of the specimens, and the specimens shall be

subjected to the dielectric test specified for’1ife cycle testing.

Oualifying activity: The activity responsible for the qualiffed products covered by this

specification sheet is Naval Avionics Center, Code 8/714, 6000 East 21st Street, Indianapolis, IN

46219-2189.

Source: https://assist.dla.mil -- Downloaded: 2018-09-14T07:51Z

Check the source to verify that this is the current version before use.

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