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MIL-N-85005A(AS)
High Level Discretes - The SC shall accept three,
3.5.7.4.4.7
high level, single-ended logic level discretes defined as follows:
0 to +4.5 VDC = Logic Zero
Open, or + 5.5 to + 15 VDC = Logic One
Input Power
3.5.7.5
Aircraft Power - The equipment shall utilize Aircraft
3.5.7.5.1
Power in accordance with Paragraph 3.3.12 as follows:
115 VAC, 400 Hz, 3 0, Category B, 430 VA
The equipment shall utilize System
System Power
3.5.7.5.2
Power as follows for a period of 10 seconds minimum (Paragraph 3.5.10)
should power interruption occur.
72 VDC to 64 VDC, 340 watts, regulated according to
power requirements, from the Computer Battery Unit.
Mounting - The NC shall be mounted on a shockmount.
3.5.7.6
The shockmount shall not be provided as part of the equipment.
Electrical Connections - Connections to external
*3.5.7.7
circuits shall be provided as listed.
Receptacle
Reference
Function
Type
Designation
Primary Power
MS27478Y14D18PA
J1
Test
SJTP02RE24-35S(023)
J2
SDC
SJTP02RE18-35P(023)
J3
SDC
SJTP02RE18-35PB(023)
J4
Keyer Control
SJTP02RE18-35SA(023)
J5
SDC
SJTP02RE18-35SC(023)
J6
Tape Loader
SJTP02RE20-35SA(023)
J7
SDC
SJTP02RE20-35P(023)
J8
Fan Power
MS27508E8F35P
J9
Color - The NC case shall be lusterless gray, No.
3.5.7.8
36231, as specified in FED-STD-595.
Signal Data Converter Unit (SDC) CV-3289/ASN-124 -
3.5.8
The SDC shall meet the following requirements:
- 98 -

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