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|  MIL-N-85005A(AS)
3.5.10.5.2
System Power - The equipment shall utilize system
power as follows:
5 VDC, 400 mAmp, regulated, from the PP-4964/ASN-84
Power Supply (not available during CMPTR)
*3.5.10.6
Mounting - The Battery Unit shall be mounted on a
shockmount (Ref. Para. 3.5.15). The shockmount shall not be supplied as
part of the equipment.
*3.5.10.7
Electrical Connections - Connections to external
circuits shall be provided as listed.
Reference
Designation
Receptacle Type
Function
J1
SJTP02RE16-35SA(023)
SDC Interface
J2
SJTP02RE14-35SB(023)
Node Controller
SJTP02RE12-35S (023)
J3
Gyro Assembly
SJTP02RE16-26P(023)
J4
Interconnecting Box
3.5.10.8
Color - The Battery unit case shall be lusterless gray,
No. 36231, as specified in FED-STD-595.
3.5.11
Mode Controller C-9856/ASN-124 - The Controller shall
meet the following requirements:
3.5.11.1
Function - The Controller shall provide the pilot
with control and monitoring of the Inertial Measurement Set (IMS) modes and
equipment status. The configuration of the front panel shall conform to
Figure 36.
3.5.11.2
Form Factor - The Mode Controller, exclusive of front
panel protrusions, attachment points, but including connector projections,
shall be formed within the following maximum dimensions (inches).
Height
Width
Depth
2.630
5.750
5.000 (behind mount-
ing surface)
3.5.11.3
Weight - The weight of the Controller shall not exceed
2 pounds.
3.5.11.4
Contents - The Controller shall contain logic circuitry
and power supplies for control and display of inertial navigation system
modes and status.
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