MS3454W36-10S Amphenol, MS3454W36-10S Datasheet - Page 6
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MS3454W36-10S
Manufacturer Part Number
MS3454W36-10S
Description
Circular MIL / Spec Connectors 48P MS Series MIL-DTL-5015
Manufacturer
Amphenol
Series
Matrix Seriesr
Datasheet
1.9440F24-10PW.pdf
(29 pages)
Specifications of MS3454W36-10S
Mil Type
MIL-DTL-5015
Product Type
Connectors
Contact Style
Socket (Female)
Shell Style
Receptacle
Shell Size
36
Number Of Contacts
48
Insert Arrangement
36-10
Mounting Style
Panel
Termination Style
Crimp
Contact Type
Socket
Shell Plating
Cadmium, Olive Drab
Current Rating
13 A
Voltage Rating
2000 V
Body Material
Aluminum
Mounting Angle
Straight
Lead Free Status / Rohs Status
Lead free / RoHS Compliant
MIL-DTL-5015 Crimp Rear Release
Insert Arrangements
F
** Inactive for new design\
• Socket only
†† A, C = Iron; B, D = Constantan
† one Iron contact and one Constantan contact
Insert Arrangement
Service Rating
Number of Contacts
Contact Size
* Consult Amphenol, Sidney, NY for availability.
Insert Arrangement
Service Rating
Number of Contacts
Contact Size
Insert Arrangement
Service Rating
Number of Contacts
Contact Size
Insert Arrangement
Service Rating
Number of Contacts
Contact Size
ront Face of Pin Insert or Rear Face of Socket Insert Illustrated
B, C, F, G = A; Bal. = Inst.
D
C
250˚
D
C
18-10**
18-16*
Contact Amphenol Aerospace for more information at 800-678-0141 • www.amphenol-aerospace.com
18-4
16
12
12
250° Rotation
D
A
4
C
1
4
F
G
E
of 18-1
18-24
H
A
B
I
J
10
16
A
B
D
A
C
B
100˚
100° Rotation
12
12
2
2
D
E
C
of 18-9
18-5 •
18-17
D
Inst.
18-11
C
F
D
12
A
5
A
B
G
E
100˚
16
16
1
C
5
100° Rotation
12
A
2
B
A
B
18-27 •
of 18-5
C
D
250˚
A
B
16
1
250° Rotation
12
2
E
D
18-6*
D
of 18-9
E
18-18
F
Inst.
D
250˚
1
4
18-12
F
C
16
A
6
G
250° Rotation
C
16
12
A
2
5
B
18-28 •
A
B
of 18-5
C
D
A
B
CONTACT LEGEND
16
1
D
C
H
1
8
B
18-19**
D
B
18-13
E
18-7*
10
16
A
A
A
B
K
1
8
F
A
20-2
12
C
J
3
G
D
1
0
Amphenol
A
18-22**
16
12
C
D
C
20-4
E
1
16
12
F
D
3
D
4
D
1
4
18-8*
18-14*
G
A
B
A
12
H
A
C
16
A
B
7
A
A, B, G, H = D; C, D, E, F = A
B
16
1
B
Aerospace
B, C, F, G = A; Bal. = Inst.
8
G
F
100° Rotation
100˚
E
F
G
of 18-1
20-7
18-23
16
E
A
H
4
H
8
10
16
12
J
I
E
2
D
D
F
18-15
18-9
Inst.
B
4††
C
12
D
D
A
A
C
G
B
A
C
C
0
A
16
5
B
B
175