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ACT4454 Datasheet(PDF) 4 Page - Aeroflex Circuit Technology

Part No. ACT4454
Description  ACT 4454 / 4460 Single Supply Transceivers for MIL-STD-1553A/B & MacAir A3818, A4905, A5232 & A5690
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Manufacturer  AEROFLEX [Aeroflex Circuit Technology]
Direct Link  http://www.aeroflex.com
Logo AEROFLEX - Aeroflex Circuit Technology

ACT4454 Datasheet(HTML) 4 Page - Aeroflex Circuit Technology

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Aeroflex Circuit Technology
SCD4454 REV A 3/17/99 Plainview NY (516) 694-6700
4
Note 2: Vcc = 5 Volts ±0.1 V, bypassed by 2.2 µF (Tantalum recommended) Capacitor minimum. All measurements &
specifications apply over the temperature range of -55°C to +125°C (case temperature) unless otherwise
specified.
Note 3: When measured at point A-A’ with ± 10 Volt peak, line to ground, DC to 2MHz
Note 4: Typical power is measured with Vbus at point A-A’ = 7.0 VP-P
Electrical Characteristics — Receiver Section
Parameter
Condition
Symbol
Min
Typ
Max
Unit
Differential Receiver Input Voltage Range
(See Figure 5, point P–P')
TXFMR 2.5:1
VIDR
14
20
VP-P
Common Mode Rejection Ratio (Note 3)
CMRR
45
dB
Strobe Characteristics (Logic "O" Inhibits Output)
"0" Input Current
VS=0.4 V
IIL
-0.2
-0.4
mA
"1" Input Current
VS=2.7V
IIH
1+40
µA
"0" Input Voltage
VIL
0.7
V
"1" Input Voltage
VIH
2.0
V
Strobe Delay (Turn-on or Turn-off)
tSD
50
100
nS
Threshold Characteristics (Sinewave Input)
Input Threshold Voltage (referred to the bus)
100KHz–1MHz
VTH
0.60
0.82
1.10
V P-P
Output Characteristics – RX DATA and RX DATA
"1" State
IOH = -0.4 mA
VOH
2.5
3.7
V
"0" State
IOL = -4.0 mA
VOL
0.35
0.5
V
Delay, (average) from Differential Input Zero
Crossings to RX DATA and RX DATA Output 50%
points
tDRX
340
500
nS
Power Data
Power Supply Currents – Per Channel
Transmitter Standby
Note 4
ICC
13
30
mA
25% duty cycle
170
200
50% duty cycle
320
400
100% duty cycle
700
800
Power Supply Voltage
Operating Power Supply Voltage Range
VCC
+4.75
+5.00
+5.50
V


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