MS3456W32-7SW Amphenol, MS3456W32-7SW Datasheet - Page 8

• Manufacturer Part Number: MS3456W32-7SW
• Description: Circular MIL / Spec Connectors 35P MS Series MIL-DTL-5015
• Manufacturer: Amphenol
• Series: Matrix Seriesr

Specifications of MS3456W32-7SW

• Mil Type: MIL-DTL-5015
• Product Type: Connectors
• Contact Style: Socket (Female)
• Shell Style: Plug
• Shell Size: 32
• Number Of Contacts: 35
• Insert Arrangement: 32-7
• Mating Style: Receptacle
• Mounting Style: Free Hanging
• Termination Style: Crimp
• Contact Type: Socket
• Shell Plating: Cadmium, Olive Drab
• Current Rating: 23 A, 13 A
• Voltage Rating: 1000 V, 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
Front Face of Pin Insert or Rear Face of Socket Insert Illustrated
** Inactive for new design
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
E
D
F
J
D
C
H
1
0
K
G
T
24-10
24-1**
S
22-14
U
22-22
Contact Amphenol Aerospace for more information at 800-678-0141 • www.amphenol-aerospace.com
A
L
7
8
19
16
G
A
D
A
4
8
M
F
A
V
N
R
12
B
1
C
A
A
P
E
A
B
B
B
D
C
D
G
3
8
A
24-11
D = 3; Bal. = A
H = D; Bal. = A
E
E
F
E
12
F
5
A
B
H
D
F
G
D
22-15*
E
22-23
24-2
12
C
12
D
12
7
8
G
6
H
A
D
I
F
16
1
C
A
C
C
A
B
B
B
D
E
2
4
24-12
J = D; Bal. = A
G
A
A = D; Bal. = A
G
F
1
0
B
12
1
8
H
F
1
H
22-27*
24-4*
22-17*
12
C
3
A
C
D
B
E
A
J
A
J
E
16
16
A
3
16
8
D
8
B
D
D
C
B
C
100˚
260˚
CONTACT LEGEND
C, D, E = A: Bal. = D
J
100° Rotation
H
16
16
F
L
L
F
K
G
260° Rotation
T
J
P
A
D
P
of 24-5
24-15
A
D
S
U
J
22-30
24-5**
F
E
of 22-14
L
A
19
16
22-18*
A
16
16
G
A
C
S
C
G
16
G
M
M
V
F
S
M
8
N
R
1
8
B
K
B
E
K
R
E
R
P
E
H
A
D
D
B
N
H
H
N
C
A
C
B
Amphenol
A, G, H = D; Bal. = A
A, B, F, G = D; C, D, E = A
260˚
12
3
16
F
E
E
260° Rotation
12
G
J
E
H
2
F
F
D
K
22-19
24-6*
G
of 22-5
22-32
P
14
16
12
A
8
D
H
24-16*
12
16
F
D
G
3
Aerospace
N
L
A
A
D
16
A
C
A
M
4
C
B
E
B
B
B
C
D
C
8
H = D; Bal. = A
12
2
J
C
B
F
E
I
K
G
G
H
12
1
0
L
2
22-36*
H
4
P
J
F
22-21
12
24-7
8
O
K
H
24-20
A
A
D
M
G
A
16
D
9
A
A
16
N
14
16
C
B
A
2
F
B
L
0
E
C
E
B
D
C
D
177