1
Contact Amphenol Aerospace for more information at 800-678-0141 • www.amphenol-aerospace.com
MIL-DTL-5015, Matrix®
TABLE OF CONTENTS FOR SECTION M
Design Characteristics, Customer Options ....................................2
Insert Availability and Identication ..........................................3, 4
Insert Arrangement Drawings ..............................................5-13
Class Descriptions, Performance Specications ................................14
Insert Alternate Positioning ................................................15
How to Order, Military and Commercial .......................................16
Shell Styles:
Wall mounting receptacle threaded MS3450 (9440) .............................17
Cable connecting receptacle threaded MS3451 (9441) ...........................18
Box mounting receptacle threaded MS3452 (9442) ..............................19
Jam nut receptacle threaded MS3454 (9444) ..................................20
Straight plug threaded MS3456 (9446) .......................................21
Straight plug, self-locking threaded MS3459 (9816) .............................22
Quick disconnect plug push-pull coupling (9817/9818) ...........................23
Matrix® 5015 with RADSOK® contacts, for high power ..........................24
Contact information, sealing plugs, tools .....................................25
Protection caps, dust caps ................................................26-28
Additional MIL-DTL-5015 connectors offered by Amphenol .......................29
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5015
MATRIX
M
2
MS3450
WALL MOUNTING
RECEPTACLE
MS3451
CABLE CONNECTING
RECEPTACLE
MS3452
BOX MOUNTING
RECEPTACLE
MS3454
JAM NUT RECEPTACLE
MS3456
PLUG WITH
THREADEDCOUPLING
MS3459
PLUG WITH
SELF-LOCKING
COUPLING NUT
AMPHENOL BROADENS THEIR MS/STANDARD
FAMILY OF CONNEC TORS WITH THE MIL-DTL-5015
CRIMP REAR RELEASE SERIES
This series provides an improved alternative to the older
MIL-C-5015 solder type. It bridges the gap between an old
connector stan dard and the environmental and high perfor-
mance needs of current technologies.
DESIGN CHARACTERISTICS
• Medium to heavy weight enviornmental cylindrical
• MS345( ) series intermateable with existing MIL-DTL-5015
solder or crimp versions on existing equipment
• Captive coupling nut mechanism, utilizes retaining rings
in combination with “L” washers to prevent inadvertent
disas sembly
• Multiple interlock systems ensure permanent
insert reten tion
• Positive control of dielectric separation with guaranteed
ease of contact insertion
• Positive contact retention provided by a closely toleranced
damage-proof metal retention clip
• Completely sealed against environmental extremes with -
• Individual contact seals (conical risers on pin interface)
• Interfacial seals between contacts
• Peripheral gasket shell-to-shell seals
• Redundant rear wire seals and insert-to-shell seals
CUSTOMER OPTIONS
• Seven mounting styles, in shell sizes 8 to 40
• Threaded coupling or self-locking plug (MS3459) with an internal
ratcheting mechanism to prevent unmating due to vibration and
shock, eliminating the need for safety wiring
• Proprietary quick disconnect plug, with or without
lanyard available
• Classes include aluminum or stainless steel shells,
or rewall capability
• Mil-Spec and custom proprietary versions available
• Some styles are supplied to McDonnell Douglas
Specica tion BAN 7025, DC60 Series
• Accommodation of contact sizes 0 to 16
• Over 100 insert arrangement patterns available,
accom modating from a minimum of 1 to a maximum
of 85 circuits
• Alternate positioning available
• High power RADSOK socket contacts available
NOTE: MIL-C-5015 is superseded to MIL-DTL-5015 for all
Amphenol/Matrix rear release crimp type contacts.
MIL-DTL-5015 with Crimp Rear Release Contacts
COMMERCIAL QUICK
DISCONNECT PLUG
WITH/WITHOUT
LANYARD
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5015 MATRIX
M
3
Amphenol Matrix 5015 Connector
With RADSOK® Contacts
FOR HIGH POWER APPLICATIONS
• Completely environmentally sealed with contact seals,
gaskets, wire seals and insert-to-shell seals
• Special design enhanced with RADSOK contacts in the plug or
receptacle instead of standard rear release crimp contacts
• All the shell styles and nishes of the Matrix 5015 family are
available, including rewall styles and non-decoupling style
• Recommended for applications up to 150° operating temperature
• Up to 40% increased current carrying capability
• RADSOK contacts provide high amperage capability with minimal
voltage loss and low insertion forces
• The RADSOK contact has a hyperbolic, stamped grid conguration
with the socket circular. As a male pin is inserted, axial members in the
female socket deect, enabling high current ow across the connection
with minimal voltage loss RADSOK
AMPHENOL’S DURMALONTM
Durmalon, like Olive-Drab Cadmium plating (Class W),
meets 500 hours of dynamic salt spray, combined with 500
mating cycles and meets specied millivolt drop shell-to-
shell conductivity. Durmalon also meets a 200° C tempera-
ture rating. Durmalon has been proven to meet this
requirement as well as Potassium Formate-Deicer uid
testing performed by Boeing.
BLACK ZINC NICKEL IS AMPHENOL’S 2ND
RoHS COMPLIANT PLATING
ALTERNATIVE TO CADMIUM
Amphenol is now offering a new RoHS compliant alternative
to Cadmium. Black Zinc Nickel is a non-reective and
conductive black nish approved for 500 hrs salt spray
making it an excellent choice for harsh environments. Black
Zinc Nickel has been qualied by the DLA. Black Zinc Nickel
is compatible with other platings and available on a wide
variety of accessories.
Standard
Contacts RADSOK Contacts
Size Amps Size Amps Cartridge size
8 46 8 70 3.6 MM
4 80 4 120 5.7MM
0 150 0 250 9.1MM
NEW RoHS FINISHES
BLACK ZINC NICKLE FINISH
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5015
MATRIX
M
4
Insert Availability and Identification
Insert
Arrangement
Service
Rating
Total
Contacts
Contact Size
0 4 8 12 16
8S-1 A 1 1
10S-2 A 1 1
10SL-3 A 3 3
10SL-4 A 2 2
12S-1 A 2 2
12S-2 A 2 2
12S-3 A 2 2
12S-4 D 1 1
12-5 D 1 1
14S-2 Inst. 4 4
14-3 A 1 1
14S-5 Inst. 5 5
14S-6 Inst. 6 6
14S-7 A 3 3
14S-9** A 2 2
14S-10 Inst. 4 4
14S-11 Inst. 4 4
14S-12 A 3 3
14S-13 A 3 3
16S-1 A 7 7
16-2* E 1 1
16S-8 A 5 5
16-9 A 4 2 2
16-10 A 3 3
16-11 A 2 2
16-12 A 1 1
16-13 A 2 2
18-1 A/Inst. 10 10
18-4 D 4 4
18-5 • D 3 2 1
18-6* D 1 1
18-8 A 8 1 7
18-9 Inst. 7 2 5
18-10** A 4 4
18-11 A 5 5
18-12 A 6 6
18-13 A 4 1 3
18-15 A 4 4
18-17 Inst. 7 2 5
18-18 Inst. 7 2 5
18-19** A 10 10
18-22** D 3 3
18-23 A/Inst. 10 10
Insert
Arrangement
Service
Rating
Total
Contacts
Contact Size
0 4 8 12 16
18-24 A/Inst. 10 10
18-27• D 3 2 1
18-28• D 3 2 1
20-2 D 1 1
20-4 D 4 4
20-7 D/A 8 8
20-8 Inst. 6 2 4
20-14 A 5 2 3
20-15 A 7 7
20-16 A 9 2 7
20-17 A 6 5 1
20-18 A 9 3 6
20-19 A 3 3
20-21 A 9 1 8
20-22 A 6 3 3
20-24 A 4 2 2
20-27 A 14 14
20-29 A 17 17
20-32 D/A 8 8
20-33 A 11 11
22-2 D 3 3
22-5 D 6 2 4
22-6* D 3 2 1
22-7* E 1 1
22-10* E 4 4
22-11* B 2 2
22-14 A 19 19
22-19 A 14 14
22-21 A 3 1 2
22-22 A 4 4
22-23 D/A 8 8
22-30 A 19 19
22-32 D 6 2 4
24-2 D 7 7
24-5** A 16 16
* Consult Amphenol Aerospace for availability
** Inactive for new design
• Socket Only
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5015 MATRIX
M
5
Insert Availability and Identification
Insert
Arrangement
Service
Rating
Total
Contacts
Contact Size
0 4 8 12 16
24-7 A 16 2 14
24-10 A 7 7
24-11 A 9 3 6
24-12 A 5 2 3
24-15 A 16 16
24-20 D 11 2 9
24-22 D 4 4
24-24 A 16 16
24-28 Inst. 24 24
28-1 D/A 9 3 6
28-2 D 14 2 12
28-9 D 12 6 6
28-10 D/A 7 2 2 3
28-11 A 22 4 18
28-12 A 26 26
28-13 A 26 26
28-15 A 35 35
28-17 B/D/A 15 15
28-19* B/D/A 10 4 6
28-20 A 14 10 4
28-21 A 37 37
28-22 D 6 3 3
32-1 E/D 5 2 3
32-6 A 23 2 3 2 16
32-7 Inst./A 35 7 28
32-9 D 14 2 12
32-13 D 23 5 18
32-15 D 8 2 6
32-16 A 23 2 3 2 16
32-17 D 4 4
32-19 E/D 5 2 3
Insert
Arrangement
Service
Rating
Total
Contacts
Contact Size
0 4 8 12 16
32-63 D 5 5
32-73 A 46 46
36-3 D 6 3 3
36-5 A 4 4
36-6 A 6 2 4
36-7 A 47 7 40
36-8 A 47 1 46
36-9 A 31 1 2 14 14
36-10 A 48 48
36-11 A 48 48
36-12 A 48 48
36-15 D/A 35 35
36-16 A 47 7 40
36-17 A 47 7 40
36-18 A 31 1 2 14 14
36-21 A 31 1 2 14 14
36-52 A 52 52
40-1 D 30 6 24
40-9 A 47 1 22 24
40-56 A 85 85
* Consult Amphenol Aerospace for availability
** Inactive for new design
Contact Amphenol Aerospace for more information at 800-678-0141 • www.amphenol-aerospace.com
5015
MATRIX
M
6
BA
BA
A
BC
D
A
B
C
D
E
FA
B
C
D
E
AB
100˚
A
BC
D
100˚
A
B
C
A
B
CD
E
F
G
A
B
C
D
E
100° Rotation
of 12S-3
250° Rotation
of 12S-3
100° Rotation
of 14S-2
250° Rotation
of 14S-2
100° Rotation
of 14S-1
260° Rotation
of 14S-1
C
BA
BA
100˚
BA
250˚
260˚
A
B
C
A
B
C
Insert Arrangement 8S-1 10S-2 10SL-3 10SL-4 12S-1 12S-2 12S-3
Service Rating A A A*** A A A A
Number of Contacts 1 1 3 2 2 2 2
Contact Size 16 16 16 16 16 16 16
Insert Arrangement 12S-4 12-5 14S-2 14-3 14S-5 14S-6
Service Rating D D Inst. A Inst. Inst.
Number of Contacts 1 1 4 1 5 6
Contact Size 16 12 16 8 16 16
Insert Arrangement 14S-7 14S-9** 14S-10 14S-11 14S-12 14S-13
Service Rating A A Inst. Inst. A A
Number of Contacts 3 2 4 4 3 3
Contact Size 16 16 16 16 16 16
Insert Arrangement 16S-1 16-2* 16S-8 16-9 16-10 16-11
Service Rating A E A A A A
Number of Contacts 7 1 5 2 2 3 2
Contact Size 16 12 16 12 16 12 12
Front Face of Pin Insert or Rear Face of Socket Insert Illustrated
* Consult Amphenol Aerospace for availability.
** Inactive for new design
*** Service rating Inst. Class K
• Socket only
† One Iron contact and one Constantan contact
AB
A
B
C
D
E
F
G
H
I
J
Insert Arrangement 16-12 16-13 18-1 18-4 18-5 • 18-6*
Service Rating A A B, C, F, G = A;
Bal. = Inst.
D D D
Number of Contacts 1 2† 10 4 2 1 1
Contact Size 4 12 16 16 12 16 4
Insert Arrangements
CONTACT LEGEND 16 12 8 4 0
A
B
C
D
B
CA
A
B
A
BC
D
A
BC
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5015 MATRIX
M
7
A
B
C
D
E
F
G
H
A
B
C
D
E
F
G
A
B
C
D
100˚
A
B
C
D
E
F
G
A
BC
DEF G
H
K
J
AB
C
* Consult Amphenol Aerospace for availability.
** Inactive for new design
• Socket only
†† A, C = Iron; B, D = Constantan
100° Rotation
of 18-9
250° Rotation
of 18-9
100° Rotation
of 18-1
A
B
C
D
E
F
G
H
I
J
100˚
250˚
A
B
C
D
E
F
G
Insert Arrangement 18-8* 18-9 18-10** 18-11 18-12 18-13
Service Rating A Inst. A A A A
Number of Contacts 1 7 2 5 4 5 6 1 3
Contact Size 12 16 12 16 12 12 16 8 12
Insert Arrangement 18-15 18-17 18-18 18-19** 18-22** 18-23
Service Rating A Inst. Inst. A D B, C, F, G = A;
Bal. = Inst.
Number of Contacts 4†† 2 5 2 5 10 3 10
Contact Size 12 12 16 12 16 16 16 16
Front Face of Pin Insert or Rear Face of Socket Insert Illustrated
250˚
A
B
C
D
E
F
G
H
I
J
A
B
D
C
A
B
C
DE
F
G
H
250° Rotation
of 18-1
100° Rotation
of 18-5
250° Rotation
of 18-5
A
BC
100˚
A
BC
250˚
Insert Arrangement 18-24 18-27 • 18-28 • 20-2 20-4 20-7
Service Rating B, C, F, G = A; Bal. = Inst. D D D D A, B, G, H = D
C, D, E, F = A
Number of Contacts 10 2 1 2 1 1 4 8
Contact Size 16 12 16 12 16 0 12 16
Insert Arrangements
CONTACT LEGEND 16 12 8 4 0
A
BC
D
A
BC
D
E
A
B
C
D
E
F
A
B
C
D
A
B
C
D
EF
A
B
C
D
E
A
B
CD
EG
F
A
B
C
D
EFG
H
I
A
BC
D
E
F
Insert Arrangement 20-8* 20-14 20-15 20-16 20-17 20-18
Service Rating Inst. A A A A A
Number of Contacts 2 4 2 3 7 2 7 5 1 3 6
Contact Size 8 16 8 12 12 12 16 12 16 12 16
A
B
C
D
E
F
G
H
I
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5015
MATRIX
M
8
A
BC
A
B
C
D
E
F
G
H
I
A
B
C
D
E
F
A
B
C
D
A
B
C
D
EF
G
H
I
J
K
L
M
N
*Consult Amphenol Aerospace for availability.
** Inactive for new design
Insert Arrangement 20-19 20-21 20-22 20-24 20-27 20-29
Service Rating A A A A A A
Number of Contacts 3 1 8 3 3 2 2 14 17
Contact Size 8 12 16 8 16 8 16 16 16
Front Face of Pin Insert or Rear Face of Socket Insert Illustrated
AB
C
D
E
F
G
H
J
K
L
MN
PT
SR
A
B
C
D
E
F
K
H
JM
L
A
BC
A
B
CD
E
F
260° Rotation of 20-7
A
B
C
DE
F
G
H
260˚
Insert Arrangement 20-32 20-33 22-2 22-5 22-6** 22-7*
Service Rating A, B, G, H = D; Bal. = A A D D D E
Number of Contacts 8 11 3 2 4 2 1 1
Contact Size 16 16 8 12 16 8 16 0
A
BC
D
AB
Insert Arrangement 22-10* 22-11* 22-14 22-19 22-21 22-22
Service Rating E B A A A A
Number of Contacts 4 2 19 14 1 2 4
Contact Size 16 16 16 16 0 16 8
Insert Arrangements
CONTACT LEGEND 16 12 8 4 0
A
B
C
D
E
F
G
H
J
K
LM
NU
V
R
S
TP
A
B
C
D
E
F
G
H
J
KL
M
N
P
A
B
C
A
BC
D
A
B
C
D
E
F
G
H
260° Rotation
of 22-5
A
B
C
D
E
F
G
H
J
K
LM
N
U
V
R
S
TP
260˚
A
B
CD
E
F
260˚
260° Rotation
of 22-14
A
B
C
A
B
C
D
E
F
G
H
260° Rotation
of 22-5
A
B
C
D
E
F
G
H
J
K
LM
N
U
V
R
S
TP
260˚
A
B
CD
E
F
260˚
Insert Arrangement 22-23 22-30 22-32 22-23 22-30 22-32
Service Rating H = D; Bal. = A A D H = D; Bal. = A A D
Number of Contacts 8 19 2 4 8 19 2 4
Contact Size 12 16 12 16 12 16 12 16
260° Rotation
of 22-14
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5015 MATRIX
M
9
*Consult Amphenol Aerospace for availability.
** Inactive for new design
Front Face of Pin Insert or Rear Face of Socket Insert Illustrated
A
B
C
D
E
F
G
AB
C
DE
FGH
JK
LMN
P
S
R
AB
C
D
E
F
G
H
J
K
L
M
N
P
IO
Insert Arrangement 24-2 24-5** 24-7 24-10 24-11 24-12
Service Rating D A A A A A
Number of Contacts 7 16 2 14 7 3 6 2 3
Contact Size 12 16 12 16 8 8 12 4 12
Insert Arrangement 24-15 24-20 24-22 24-24 24-28 28-1
Service Rating A D D A Inst. A, J, E = D;
Bal. = A
Number of Contacts 16 1 9 4 16 24 2 7
Contact Size 16 8 16 8 16 16 12 6
AB
C
D
EF
G
H
J
KL
100° Rotation
of 24-5
AB
C
DE
FGH
JK
LMN
PS
R
100˚
Insert Arrangements
CONTACT LEGEND 16 12 8 4 0
A
B
CD
E
F
G
ABC
DEF
G
H
I
A
B
C
D
E
A
BC
D
ABCD
EFGH J
KL
M
NPQ
RST
U
V
WX YZ
AB
C
DE
FGH
JK
LMN
P
S
R
250˚
250° Rotation
of 24-5
AB
C
D
E
F
G
H
J
A
B
C
D
EF
G
H
J
K
L
M
N
P
AB
CD
P
S
EFG
Insert Arrangement 28-2 28-4* 28-9 28-10 28-11
Service Rating D G, P, S = E; Bal. = D D G = D, Bal. = A A
Number of Contacts 2 12 2 7 6 6 2 2 3 4 18
Contact Size 12 16 12 16 12 16 4 8 12 12 16
A
B
C
DE
F
G
H
J
K
LM
A
B
CD
E
F
G
A
B
C
D
E
F
G
H
J
K
L
M
I
N
P
R
S
T
U
V
W
X
A
B
C
D
E
F
G
H
J
K
L
M
PR
N
S
T
U
V
W
X
Y
Z
a
b
d
100˚
A
B
C
D
E
F
G
H
J
K
L
M
PR
N
S
T
U
V
W
X
Y
Z
a
b
d
AB
CDEFG
HJKLM
PRS T
N
W
XYZ
UV
abc
d
e
f
g
h
jk
m
l
A
B
CD
E
F
G
HJK
L
M
N
P
R
100° Rotation
of 28-12
Insert Arrangement 28-12 28-13 28-15 28-17 28-19*
Service Rating A A A R = B; M, N, P = D;
Bal. = A
H, M = B; A, B = D;
Bal. = A
Number of Contacts 26 26 35 15 4 6
Contact Size 16 16 16 16 12 16
AB
C
E
G
H
J
K
L
M
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5015
MATRIX
M
10
A
B
C
D
E
F
G
H
J
K
L
M
N
P
A
BC
D
EFGHJ
KLMNPR
STUVWXZ
abcdef
ghjkm
nprs
Insert Arrangement 28-20 28-21 28-22 32-1 32-6
Service Rating A A D A = E; B, C, D, E = D A
Number of Contacts 10 4 37 3 3 2 3 2 3 2 16
Contact Size 12 16 16 4 16 0 12 4 8 12 16
Front Face of Pin Insert or Rear Face of Socket Insert Illustrated
A
B
C
DE
F
A
B
CD
E
AB
CD
EF
GH
J
KLMN
O
PR
S
T
UV
W
I
X
A
B
C
D
E
F
G
H
I
J
K
L
M
N
O
P
R
S
T
U
V
W
X
Y
Z
a
b
c
d
e
f
g
h
j
k
AB
CD EFG
HI JK
LMN
A
B
C
D
E
F
G
H
J
K
L
M
N
P
R
S
T
U
V
W
X
Y
Z
A
BC
DE
F
G
H
100˚
AB
CD
EF
GH
IJ
KLM N
O
PR
S
T
UV
WX
A
BC
D
100° Rotation
of 32-6
260° Rotation
of 32-1
CD
E
260˚
B
A
Insert Arrangement 32-7 32-9 32-13 32-15
Service Rating A, B, h, j = Inst.; Bal. = A D D D
Number of Contacts 7 28 2 12 5 18 2 6
Contact Size 12 16 4 16 12 16 0 12
Insert Arrangement 32-16 32-17 32-19 32-63
Service Rating A D A = E, Bal. = D D
Number of Contacts 2 3 2 16 4 2 3 5
Contact Size 4 8 12 16 4 0 12 4
Insert Arrangements
CONTACT LEGEND 16 12 8 4 0
A
B
C
D
E
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5015 MATRIX
M
11
AB
CDE
FG
HIJ
KLMN
OPRST
UVW X
YZab c
defg
hjkm
np
r
t
s
uv
xy
z
w
A
BC
DE
F
GH
IJKL
M
NOPR
STU
V
WX
Y
Za
bcde
fg hj
k
m
npr
t
u
vw
s
xy
z
A
B
C
D
E
F
G
H
I
J
K
L
M
N
O
P
R
S
T
U
V
W
X
Y
Z
a
b
c
d
e
f
AB
CD EFG
HJKLMN
OPQR ST U
VWXYZabc
de fg hj k
mnpr
tuvw
s
x
yz
q
100˚
AB
CD EFG
HJKLMN
OPQRSTU
VWXY Zabc
def g hj k
mnpr
tuvw
s
x
yz
q
100° Rotation
of 36-10
Insert Arrangement 32-73 36-3 36-5 36-6
Service Rating A D A A
Number of Contacts 46 3 3 4 2 4
Contact Size 16 0 12 0 0 4
Insert Arrangement 36-7 36-8 36-9 36-10
Service Rating A A A A
Number of Contacts 7 40 1 46 1 2 14 14 48
Contact Size 12 16 12 16 4 8 12 16 16
Insert Arrangement 36-11 36-12 36-15 36-16
Service Rating A A M = D, Bal. = A A
Number of Contacts 48 48 35 7 40
Contact Size 16 16 16 12 16
Front Face of Pin Insert or Rear Face of Socket Insert Illustrated
Insert Arrangements
CONTACT LEGEND 16 12 8 4 0
A
B
C
D
E
F
A
B
C
D
A
B
C
D
E
F
1
2
3
4
5
6
7
8
9
1011
12
13
14
15
16
17
18
19
20 21
22
23
24
25
26
27
28
29
30
31
32
33
34
35
36
37
38
39
40
41
42
43
44
45
46
110˚
AB
CD EFG
HJ KLMN
OPQR STU
VWXY Zabc
de fg hjk
mnpr
tu vw
s
x
yz
q
A
B
C
D
E
F
G
H
J
K
L
M
N
P
Q
R
S
T
U
V
W
X
YZ
a
b
c
d
e
f
gh
j
k
m
100˚
AB
CDE
FG
HIJ
KLMN
OPRS
T
UVWX
YZabc
defg
hjkm
np
r
t
uv
w
s
xy
z
110° Rotation of
36-10
100° Rotation
of 36-7
Contact Amphenol Aerospace for more information at 800-678-0141 • www.amphenol-aerospace.com
5015
MATRIX
M
12
110˚
AB
CDE
FG
HIJ
KLMN
OPRST
UVWX
YZabc
defg
hjkm
np
r
t
uv
w
s
xy
z
100˚
A
B
C
D
E
F
G
H
I
J
K
L
M
N
O
P
R
S
T
U
V
W
X
Y
Z
a
b
c
d
e
f
ABC
D
EFHJ
K
LM NPRS
TUVWXY Z
abcdfghi
jkmn pr
tuvw
sx
yz
q
AA AB AC
AD
AE AF
AH
ABC
DE FG
HI JKL
MNOPRS
TU VWX
YZ ab
cde
* Consult Amphenol Aerospace for availability.
100° Rotation
of 36-9
260° Rotation
of 36-9
A
B
C
D
E
F
G
H
I
J
K
L
M
N
O
P
R
S
T
U
V
W
X
Y
Z
a
b
c
d
e
f
260˚
Front Face of Pin Insert or Rear Face of Socket Insert Illustrated
Insert Arrangement 36-18 36-21 36-52 36-17
Service Rating A A A A
Number of Contacts 1 2 14 14 1 2 14 14 52 7 40
Contact Size 4 8 12 16 4 8 12 16 16 12 16
Insert Arrangement 40-1 40-5* 40-9 40-56
Service Rating D A A A
Number of Contacts 6 24 3 2 4 6 1 22 24 85
Contact Size 12 16 0 4 8 2 6 12 16 16
Insert Arrangements
CONTACT LEGEND 16 12 8 4 0
A
B
C
D
E
F
G
H
I
J
K
L
M
N
O
AB
CDE
F
GHIJ
KL
MN OPQ
RST
UVWXYZa
bcd
efg h i
jk
lm
n
p
r
tu
s
o
q
ABCD
EF HJ KLM
NPRSTUVW
XYZabcdfg
hijkmn pr
tuvw
s
xyz
q
AA AB
AC AD AE AF AH AJ AK AL AM AN
AP AR AS AT
AU AV AW AX AY
AZ BA BB
BV
BC BD BE BF BH
BJ BK BL BM BN
BS BT BU
BP BR
110° Rotation of
36-7
Contact Amphenol Aerospace for more information at 800-678-0141 • www.amphenol-aerospace.com
5015 MATRIX
M
13
Class Descriptions, Performance Specifications
CLASS DESCRIPTIONS
MILITARY MIL-DTL-5015
Class L* Aluminum shell, electroless nickel nish,
uid resistant insert
Class W Aluminum shell, cadmium olive drab nish,
uid resistant insert
Class LS Stainless steel shell, passivated, uid
resistant insert
Class KT** Firewall, steel shell, cadmium olive drab nish, non-
ammable hard dielectric and uid resistant insert
Class KS Firewall, stainless steel shell, passivated, non-
amma ble hard dielectric and uid resistant insert
* Class L inactivates older Class U (aluminum, electroless nickel)
** Class KT (ferrous alloy, cadmium/olive drab) inactivates older Class K
(ferrous alloy, electroless nickel)
AMPHENOL/MATRIX
Class A Aluminum shell, black anodize nish,
uid resistant insert
Class F Aluminum shell, electroless nickel nish,
uid resistant insert
Class W Aluminum shell, cadmium/olive drab nish,
uid resistant insert
Class FS Stainless steel shell, passivated, uid resistant insert
Class KT Firewall, steel shell, cadmium olive drab nish, non-
ammable hard dielectric and uid resistant insert
Class KS Firewall, stainless steel shell, passivated,
non-amma ble hard dielectric and uid resistant insert
Class DT Aluminum shell, Durmalon (Nickle PTFE)
Class DZ Aluminum shell, Black Zinc Nickel*
* Not available in size 36 or 40
VOLTAGE RATING
Altitude Inst. A D E B C
Sea Level 1000 2000 2800 3500 4500 7000
50,000 ft. 400 600 675 750 825 975
70,000 ft. 260 360 400 440 480 560
110,000 ft. 200 200 200 200 200 200
PERFORMANCE SPECIFICATIONS
SHOCK
Wired, mated connectors are subjected to one shock in each of three mutu ally
perpendicular axes with pulse of an approximate half sine wave of 50g magnitude for a
duration of 11 milliseconds. All contacts wired in series cir cuit with 100 ±10
Milliamperes of current ow.
OPERATING TEMPERATURE RANGE
Classes L, LS and KS have temperature range of
–55°C (–75°F) to 200°C (392°F)
Classes W and KT have temperature range of
–55°C (–75°F) to 175°C (347°F)
ENVIRONMENTAL SEAL
Wired, mated connectors with the specied accessory attached will meet the
altitude immersion test specied in MIL-DTL-5015.
DURABILITY
Minimum of 100 mating cycles.
Contact Amphenol Aerospace for more information at 800-678-0141 • www.amphenol-aerospace.com
5015
MATRIX
M
14
To avoid cross-plugging problems in applications requiring the
use of more than one connector of the same size and arrange-
ment, alternate rotations are available as indicated in the
accompanying charts.
As shown in the diagram below, the front face of the pin insert is
rotated within the shell in a clockwise direction from the normal
shell key. The socket insert would be rotated counter-clockwise
the same number of degrees in respect to the normal shell key.
The charts give the W, X, Y, Z positions for the alternate rotations
available for the insert arrangements of the rear release
MIL-DTL-5015 series of connectors. If an insert arrangement
number is not given, then there is no available alternate rotation
for that pattern.
AB
AB
A
B
A
B
The following insert arrangements have the same alternate
insert rotations for W, X, Y and Z, which are:
Degrees
W X Y Z
80 110 250 280
16-7 20-22 24-4 28-4 28-21 40-3
18-5 22-6 24-5 28-8 32-1 40-4
18-9 22-12 24-6 28-9 32-3 40-5
18-13 22-14 24-7 28-10 32-6 40-6
18-14 22-15 24-12 28-11 32-9 40-7
20-7 22-17 24-16 28-15 32-13 40-11
20-8 22-18 24-20 28-16 32-22
20-9 22-19 24-21 28-17 36-7
20-14 22-21 24-28 28-19 36-8
20-16 24-1 28-1 28-20 40-2
Insert
Arrangement
Degrees
W X Y Z
12S-3 70 145 215 290
14S-2 – 120 240 –
14S-5 – 110 – –
14S-7 90 180 270 –
14S-9 70 145 215 290
16S-1 80 – – 280
16S-4 35 110 250 325
16S-8 – 170 265 –
16-9 35 110 250 325
16-10 90 180 270 –
16-11 35 110 250 325
16-13 35 110 250 325
18-1 70 145 215 290
18-4 35 110 250 325
18-8 70 – – 290
18-10 – 120 240 –
18-11 – 170 265 –
18-12 80 – – 280
18-15 – 120 240 –
18-19 – 120 240 –
18-22 70 145 215 290
20-4 45 110 250 –
20-15 80 – – 280
Insert
Arrangement
Degrees
W X Y Z
20-17 90 180 270 –
20-18 35 110 250 325
20-19 90 180 270 –
20-21 35 110 250 325
20-24 35 110 250 325
20-27 35 110 250 325
20-29 80 – – 280
22-2 70 145 215 290
22-4 35 110 250 325
22-5 35 110 250 325
22-9 70 145 215 290
22-10 35 110 250 325
22-11 35 110 250 325
22-22 – 110 250 –
22-23 35 – 250 –
22-27 80 – 250 280
22-36 90 – 270 –
24-2 80 – – 280
24-10 80 – – 280
24-11 35 110 250 325
24-22 45 110 250 –
24-27 80 – – 280
24-80 35 145 240 300
Insert
Arrangement
Degrees
W X Y Z
28-2 35 110 250 325
28-3 70 145 215 290
28-5 35 110 250 325
28-12 90 180 270 –
28-18 70 145 215 290
28-22 70 145 215 290
32-2 70 145 215 290
32-7 80 125 235 280
32-15 35 110 250 280
32-17 45 110 250 –
32-73 36 – – –
36-3 70 145 215 290
36-5 – 120 240 –
36-6 35 110 250 325
36-9 80 125 235 280
36-10 80 125 235 280
36-15 60 125 245 305
36-52 72 144 216 288
36-66 110 250 260 280
40-1 65 130 235 300
40-9 65 125 255 310
40-10 65 125 255 310
40-56 72 144 216 288
40-62 30 130 220 290
Insert Alternate Positioning
Position W Position X Position Y Position Z
View looking into front face of pin insert or rear of socket insert.
Contact Amphenol Aerospace for more information at 800-678-0141 • www.amphenol-aerospace.com
5015 MATRIX
M
15
NEW
NEW
How to Order
1. 2. 3. 4. 5. 6. 7.
MIL-DTL-5015 with rear
release crimp contacts
Connector
Type
Shell
Style
Service
class
Shell Size–
Insert Arrangement
Contact
Types
Alternate
Positions
Modification
Number
MILITARY MS 3456 L 16S–8 P W NA
COMMERCIAL 944 6 F 16S–8 P W (XXX)
2. SHELL STYLE - THREADED COUPLING
3450 Wall mounting receptacle
3451 Cable connecting receptacle
3452 Box mounting receptacle
3454 Jam nut receptacle
3456 Straight plug
3459 Straight plug with self-locking coupling nut
1. MILITARY CONNECTORY TYPE
MS Designates Military Standard
3. SERVICE CLASS
LAluminum shell, electroless nickel nish,
uid resis tant insert
WAluminum shell, cadmium olive drab nish,
uid resistant insert
LS Stainless steel shell, passivated, uid resistant insert
FIREWALL STYLES ONLY AVAILABLE FOR
3450, 3456, 3459 PER MIL SPEC:
KT Firewall, steel shell, cadmium/olive drab nish, non-
ammable hard dielectric and uid resistant insert
KS Firewall, stainless steel shell, passivated, non-am-
mable hard dielectric and uid resistant insert
4. SHELL SIZE & INSERT ARRANGEMENT
SEE PAGES 3-13
First number represents Shell Size,
second number is the Insert Arrangement.
5. CONTACT TYPE
PPin
SSocket
ALess pins
BLess sockets
Note: Class L inactivates older Class U.
Class K is inactive and has been replaced by Class KT
for all applications.
6. ALTERNATE POSITIONS
“W”, “X”, “Y”, “Z” designate that insert is rotated in its shell
from normal position. No letter required for normal
(no rotation) position. See page 15 for description of
alternate positions.
2. SHELL STYLE - THREADED COUPLING
0Wall mounting receptacle
1Cable connecting receptacle
2Box mounting receptacle
4Jam nut receptacle
6Straight plug
2. SELF LOCKING/QUICK DISCONNECT (981)
6Straight plug with self-locking coupling nut
7Quick disconnect plug with lanyard
8Quick disconnect plug without lanyard
1. COMMERCIAL CONNECTOR TYPE
944 Designates Amphenol/Matrix Commercial Series
981 Designates self locking/Quick disconnect (+)(-) lanyard
3. SERVICE CLASS
AAluminum shell, black anodize nish,
uid resistant insert (not MIL-Spec)
FAluminum shell, electroless nickel nish,
uid resis tant insert
WAluminum shell, cadmium olive drab nish,
uid resistant insert
FS Stainless steel shell, passivated,
uid resistant insert
RS Fluid resistant insert
KT Firewall, steel shell, cadmium/olive drab nish,
non-ammable hard dielectric and uid resistant insert
KS Firewall, stainless steel shell, passivated,
non-am mable hard dielectric and uid resistant insert
DT Aluminum shell, Durmalon (Nickle PTFE)
DZ Aluminum shell, Black Zinc Nickel*
* Not available in size 36 or 40
5. CONTACT TYPE
PPin
SSocket
6. ALTERNATE POSITIONS
“W”, “X”, “Y”, “Z” designate that insert is rotated in its shell
from normal position. No letter required for normal
(no rotation) position. See page 15 for description of
alternate positions.
Consult Amphenol Aerospace for information.
For strain reliefs use the following modication codes:
(189) E-nut M85049/31 conguration
(190) Straight strain relief M85049/52 conguration
(191) 90° strain relief M85049/51 conguration
(988) RADSOK sockets (sizes 0-8 guage only)
7. MODIFICATION NUMBER
4. SHELL SIZE & INSERT ARRANGEMENT
SEE PAGES 3-13
First number represents Shell Size,
second number is the Insert Arrangement.
NEW