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|  MIL-N-85005A(AS)
3.5.9.3
Weight - The weight of the Radar Buffer Converter shall
not exceed 1.5 pounds.
3.5.9.4
Contents - The Radar Buffer Converter shall contain
the circuits necessary to develop Range Gate Bar and Scale Factor Gate
Bar outputs for the SDC from inputs of Strobe and Scale Factor Gate from
the IP-414A/APA-125 Radar Indicator in accordance with MIL-I-19165.
The Buffer outputs shall not be adversely affected when cursor 3 is
active.
3.5.9.5
Mounting - The Radar Buffer Converter shall be
designed to mount in any attitude. Mounting dimensions shall be per
Figure 35.
Color - The case of the Radar Buffer Converter shall
3.5.9.6
be lusterless gray, No. 36231 per FED-STD-595.
*3.5.9.7
Electrical Connections - Connections to external
circuits shall be provided as listed.
Reference
Receptacle Type
Function
Designation
M39012/24-0001
Range Strobe Input
J1
SJTP02RE8-35S(023)
J2
Range S.F. Gate Input
SJTP02RE10-35P(023)
J3
Range Output and
Power Input
Aircraft Power - The equipment shall utilize aircraft
3.5.9.8
power in accordance with Paragraph 3.3.12 as follows:
115 V, 400 Hz, 1 0, 0.1 Amp
3.5.10
Battery Unit BA-597/ASN-124 - The Battery Unit shall
meet the following requirements:
Function - The Battery Unit shall provide battery
3.5.10.1
power to the NC during power interruptions and shall provide sequencing
and interlock circuits for control of the Inertial Measurement System
AN/ASN-84.
Form Factor - The Battery Unit, including connectors,
3.5.10.2
shall be formed within the following maximum dimensions (inches).
Width
Depth
Height
6.500
13.000
8.500
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