MS3456L22-2S Amphenol, MS3456L22-2S Datasheet - Page 6

• Manufacturer Part Number: MS3456L22-2S
• Description: Circular MIL / Spec Connectors 3P MS Series MIL-DTL-5015
• Manufacturer: Amphenol
• Series: Matrix Seriesr

Specifications of MS3456L22-2S

• Mil Type: MIL-DTL-5015
• Product Type: Connectors
• Contact Style: Socket (Female)
• Shell Style: Plug
• Shell Size: 22
• Number Of Contacts: 3
• Insert Arrangement: 22-2
• Mating Style: Receptacle
• Mounting Style: Free Hanging
• Termination Style: Crimp
• Contact Type: Socket
• Shell Plating: Nickel, Electroless
• Current Rating: 46 A
• Voltage Rating: 2800 V
• 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