MS3450W20-18S Amphenol, MS3450W20-18S Datasheet - Page 5
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MS3450W20-18S
Manufacturer Part Number
MS3450W20-18S
Description
Circular MIL / Spec Connectors 9P MS Series MIL-DTL-5015
Manufacturer
Amphenol
Series
Matrix Seriesr
Datasheet
1.9440F24-10PW.pdf
(29 pages)
Specifications of MS3450W20-18S
Mil Type
MIL-DTL-5015
Product Type
Connectors
Contact Style
Socket (Female)
Shell Style
Receptacle
Shell Size
20
Number Of Contacts
9
Insert Arrangement
20-18
Mounting Style
Panel
Termination Style
Crimp
Contact Type
Socket
Shell Plating
Cadmium, Olive Drab
Current Rating
23 A, 13 A
Voltage Rating
2000 V
Body Material
Aluminum
Mounting Angle
Straight
Lead Free Status / Rohs Status
Lead free / RoHS Compliant
174
Contact Amphenol Aerospace for more information at 800-678-0141 • www.amphenol-aerospace.com
F
** Inactive for new design
*** Service rating Inst Class K
† one Iron contact and one Constantan contact
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
Insert Arrangement
Service Rating
Number of Contacts
Contact Size
* Consult Amphenol, Sidney, NY for availability
Insert Arrangement
Service Rating
Number of Contacts
Contact Size
ront Face of Pin Insert or Rear Face of Socket Insert Illustrated
Amphenol
Aerospace
12
2
D
E
D
12S-4
C
14S-7
F
16S-1
8S-1
16-9
B
16
G
16
16
16
A
D
A
A
A
1
1
3
7
A
C
A
A
C
16
2
B
B
MIL-DTL-5015 Crimp Rear Release
Insert Arrangements
10S-2
14S-9**
C
16-10
12-5
16-2*
16
12
A
B
1
D
12
1
16
A
3
A
12
2
E
1
A
B
A
14S-1**
100° Rotation
10SL-3
100˚
B
A***
C
16
of 14S-2
16
C
14S-10
A
3
3
16-11
D
C
16S-3*
A
Inst.
B
A
12
16
A
2
4
16
B
1
A
B
A
B
CONTACT LEGEND
10SL-4
250˚
D
C
14S-2
Inst.
250° Rotation
16
16
A
A
2
4
B
of 14S-2
D
C
14S-11
16-12
Inst.
A
B
B
16
16S-4*
A
1
4
4
16
D
2
A
B
A
100° Rotation
100˚
of 12S-3
12S-1
B
14-3
16
A
2
A
1
8
B
A
16-13
16
100° Rotation
100˚
2†
12
A
1
8
of 14S-1
14S-12
C
16-7*
A
16
B
A
3
A
A
12
B
C
A
250˚
250° Rotation
16
2
of 12S-3
B, C, F, G = A; Bal. = Inst.
D
12S-2
E
14S-5
Inst.
B
8
16
16
A
2
C
5
A
A
B
F
G
260˚
E
H
18-1
260° Rotation
D
I
J
10
16
4
C
16S-8
of 14S-1
14S-13
16
A
5
C
16
D
A
A
3
E
E
A
B
C
12S-3
14S-6
B
F
D
Inst.
B
B
A
16
16
A
2
6
A
0
A
C
B