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ACT4419D Datasheet(PDF) 5 Page - Aeroflex Circuit Technology

Part No. ACT4419D
Description  Dual Variable Amplitude Transceivers for MIL-STD-1553
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Manufacturer  AEROFLEX [Aeroflex Circuit Technology]
Direct Link  http://www.aeroflex.com
Logo AEROFLEX - Aeroflex Circuit Technology

ACT4419D Datasheet(HTML) 5 Page - Aeroflex Circuit Technology

  ACT4419D Datasheet HTML 1Page - Aeroflex Circuit Technology ACT4419D Datasheet HTML 2Page - Aeroflex Circuit Technology ACT4419D Datasheet HTML 3Page - Aeroflex Circuit Technology ACT4419D Datasheet HTML 4Page - Aeroflex Circuit Technology ACT4419D Datasheet HTML 5Page - Aeroflex Circuit Technology ACT4419D Datasheet HTML 6Page - Aeroflex Circuit Technology  
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Aeroflex Circuit Technology
SCD4419D REV G 5/10/00 Plainview NY (516) 694-6700
5
Configurations and Ordering Information
Model No.
DESC No.
Receiver Data level
Case
Specs.
Configuration
ACT4419-D *
Pending
Normally Low
DIP
1553
Dual
ACT4419-DF *
Pending
Normally Low
Flat Package
1553
Dual
* For 10V Control voltage consult factory.
Figure 4 – Transmitter (TX) Output Offset
Figure 5 – Typical Transformer Connection
OUTPUT OFFSET
*
OUTPUT OFFSET
*
LAST BIT
2.5 µsec
*Offset measured at point A-A’ in Figure 5
1:2.5
A
A’
B’
B
TX DATA OUT
TX DATA OUT
RX DATA IN
RX DATA IN
70
70
55
55
Center
Tap
1:1.77 for
stub
coupling
Magnified View
D.U.T
P’
P
ZO
Use Technitrol 1553-45 or Equivalent
Transformer:
VCONT = 0 – 5Vdc
(Total hybrid with one channel transmitting
and the other in standby)
0.4FS
0.8FS
0.6FS
0.2FS
VO PK-PK @ A–A'
FS
Figure 6 – Power Dissipation vs. Duty Cycle
Note: Vcc = 5 Volts, Vbus (Pt. A-A') at 7.1 Volts P-P
0
10
20
30
40
50
60
70
80
90 100
1600
1400
1200
1000
800
600
400
200
0
DUTY CYCLE – PERCENT
Typical
Maximum
Figure 3 – Transmitter Output Amplitude (VO)
vs VCONT Voltage
0
1
2
3
4
5
CONTROL VOLTAGE
2.84
7.1
5.68
4.26
1.42
0
VCONT dc
Slope =
VO ÷ ∆VCONT


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