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MIL-N-85005A(AS)
Input Power
3.5.4.7
Aircraft Power - The equipment shall utilize aircraft
3.5.4.7.1
power in accordance with Paragraph 3.3.12 as follows:
(1) 0-26 VAC, 400 Hz, 10, 0.5 Amp.
26 VAC, 400 Hz, 10, 1.8 Amps
(2)
System Power - The equipment shall utilize system
3.5.4.7.2
power from the SDC as follows:
(1) +13.5 VDC, nominal 550 mAmp, regulated, 10%
(2) -13.5 VDC, nominal 550 mAmp, regulated, 10%
5.2 VDC, nominal 2.5 Amp, regulated 5%
(3)
*3.5.4.8
Electrical Connections - Connections to external
circuits shall be provided as follows:
Function
Receptacle Type
Reference Designation
Logic Power
M81511/51F-E-03P2
J1
Lighting Power
SJTP02RE10-5P(023)
J2
Video Output
DAGE 4679-1
J3
Horiz. Deflection
DAGE 4679-1
J4
Vert. Deflection
DAGE 4679-1
J5
Data and Discretes
SJTP02RE14-35PC(023)
J6
Blanking
DAGE 4679-1
J7
Test
SJTP02RE18-35P(023)
J8
Mounting - The Control shall meet the requirements
3.5.4.9
of MIL-C-6781 for Type I control panels.
Color - The surface shall be painted lusterless
3.5.4.10
black, No. 37038, in accordance with FED-STD-595.
Converter-Interface CV-3332/ASN-124 - The Converter
3.5.5
shall meet the following requirements.
Function - The Converter shall provide the TACCO
3.5.5.1
with readouts of RF channels and the bearings or ranges from Traces U
and L, Grams I, II, III, and IV of both Sensor Stations. It shall provide
interface with an IP-886B/ASA-66 Display. It shall provide controls to
update the bearing or range data displayed on the IP-886B/ASA-66 Tactical
Display.  The front panel of the unit shall conform to Figure 21.
Interface signal flow is shown in the block diagram of Figure 22. The
Converter-Interface and the Tactical Display Control, together, make up
the Integrated Tactical Display System (ITADS).
Form Factor - The Converter, exclusive of front
3.5.5.2
panel protrusions, attachment points, fan and connector projections,
shall be formed within the following maximum dimensions (inches).
Depth
Width
Height
18.000 (behind front panel)
9.000
16.4
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