D20419-80 Datasheet, PDF (385/386 Pages) ITT Industries – Military/Aerospace

D Subminiature
Panel Mounting
Pin Front Mounting
Pin Rear Mounting
PIN
B
A
SOCKET
Socket Front Mounting
Socket Rear Mounting
Figure 1A
Pin Front Mounting
.187 (4.75) MAX. ROLL
OVER TYPICAL
H
Socket Front Mounting
Pin Rear Mounting
PIN
C
SOCKET
Socket Rear Mounting
Figure 1B
Pin Rear Mounting
F
PIN
A
SOCKET
.145 (3.70) MAX. ROLL
OVER TYPICAL
Socket Float Mounting
Pin Front Mounting
C
RIVET
.031 (0.80) NOM. THICK
WASHER
.031 (0.80) NOM. THICK
Socket Float Mounting
Figure 2
Pin Rear Mounting
PIN
C
SOCKET
Socket Reverse
Float Mounting
RIVET
Figure 3
Pin Front Mounting
WASHER
B
Socket Reverse
Float Mounting
Combination of Mated Connectors
Fig. No. Size Pin (See Note Below) Socket
1 A, E
Standard
Standard
A
+ .030 (+0.76)
-.000 (-0)
.250 (6.35)
1 B, C, D Standard
Standard
.238 (6.04)
2 A, E
Standard
Float Mount
.218 (5.53)
2 B, C, D Standard
Float Mount
.206 (5.23)
2 A, E
Float Mount
Standard
.218 (5.53)
2 B, C, D Float Mount
Standard
.206 (5.23)
3 A, E
Standard
Rev. Float Mount
-
3 B, C, D Standard
Rev. Float Mount
-
3 A, E
Rev. Float Mount Standard
-
3 B, C, D Rev. Float Mount Standard
-
B
+ .030 (+0.76)
-.000 (-0)
C
+ .030 (+0.76)
-.000 (-0)
.340 (8.63)
.295 (7.49)
.343 (8.71)
.298 (7.56)
-
.263 (6.68)
-
.266 (6.75)
-
.263 (6.68)
-
.251 (6.37)
.358 (9.09)
.313 (7.95)
.361 (9.16)
.301 (7.64)
.358 (9.09)
.313 (7.95)
.355 (9.01)
.310 (7.87)
F
+_.010 (+_.025)
-
-
.120 (3.04)
.120 (3.04)
.120 (3.04)
.130 (3.30)
.120 (3.04)
.120 (3.04)
.120 (3.04)
.130 (3.30)
H
+ .030 (+0.76)
-.000 (-0)
.295 (7.49)
.283 (7.18)
-
-
-
-
-
-
-
-
NOTE:
1. A, B, C and H are dimensions betwen panels and represent the
recommended limit to be used in the design of the connector
mounting method.
2. It is recommended that only one assembly, either pin or socket,
be float mounted.
3. Standard pin assemblies contained .015 (0.38) thick front
shells on E and A sizes; .024 (.061) thick front shells on B, C,
and D sizes.
4. Standard connectors accommodate a #4 screw. Float mount
connectors accommodate a #2 screw.
MIL-C-24308 Test Extracts Applicable to Class G Connectors
Test Descriptions
Mating/Unmating Force
Contact Retention
Insulation
Resistance
Contact Resistance
Vibration
Shock
Durability
Salt Spray
(Corrosion)
Fluid Immersion
Shell Size
1
2
3
4
5
Requirement
Max Unmating (LBS)
6
10
17
24
30
Max Mating (LBS)
10
17
28
39
49
Contacts shall be retained in their inserts by a 9 pound (minimum) force. The axial displacement of contacts shall not exceed
.012 inch while under load.
After humidity 1 Megohm (min)
All othe condidtions 5000 Megohm (mm).
After salt spray not to exceed 55 millivolts max.
No damage and no loosening of parts due to vibration. No interruption of eletrical continulty longer than 1 microsecond.
No damage and no loosening of parts. No interruption of eletrical continulty longer than 1 microsecond.
No electrial or mechanical defects after 500 cycles of mating and unmating
No exposure of base metal due to corrosion which will affect performance. Product will meet further test as specified.
20 hours. immersion MIL-H-5606 Hydraulic Fluid
20 hours, immersion MIL-L-23659 Lubricating Fluid
Connectors shall meet mating/unmating force following immersion.
Method
MIL-STD-1344
Method 2013
MIL-STD-1344
Method 2004
MIL-STD-1344
Method 3003
#20 AWG, 7.5 Amp
MIL-STD-1344
Method 3004
MIL-STD-1344
Method 2005 Test Cond. 4
MIL-STD-1344
Method 2004 Test Cond. E
MIL-STD-1344
Method 2016
200 +_ 100 cycles/hour
MIL-STD-1344
Method 1001 Cond. B
MIL-STD-1344
Method 1016
Dimensions are shown in inches (millimeters).
Dimensions subject to change.
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