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ACT4808N Datasheet(PDF) 4 Page - Aeroflex Circuit Technology

Part # ACT4808N
Description  Dual Transceivers for MACAIR (A3818, A4905, A5232, A5690) and MIL-STD-1553A/B
PDF  9 Pages
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Manufacturer  AEROFLEX [Aeroflex Circuit Technology]
Direct Link  http://www.aeroflex.com
Logo AEROFLEX - Aeroflex Circuit Technology

ACT4808N Datasheet(HTML) 4 Page - Aeroflex Circuit Technology

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4
SCD4808N Rev B
ELECTRICAL CHARACTERISTICS – RECEIVER SECTION
Parameter
Condition
Symbol
Min
Typ
Max
Unit
Differential Input Impedance
f = 1MHz
ZIN
10K
-
-
Ω
Differential Input Voltage Range
-
VIDR
--
40
Vp-p
Input Common Mode Voltage Range
-
VICR
10
-
-
Vp-p
Common Mode Rejection Ratio
-
CMRR
40
-
-
dB
STROBE CHARACTERISTICS (LOGIC "0" INHIBITS OUTPUT)
"0" Input Current
VS = 0.4 V
IIL
-
-0.2
-0.4
mA
"1" Input Current
VS = 2.7 V
IIH
-1.0
+40
µA
"0" Input Voltage
-
VIL
--
0.7
V
"1" Input Voltage
-
VIH
2.0
-
-
V
Strobe Delay (Turn-on or Turn-off)
-
tSD
-
40
150
nS
THRESHOLD CHARACTERISTICS (SINEWAVE INPUT )
Internal Threshold Voltage Figure 4
Point B-B’
1MHz
VTH
0.60
0.80
1.10
Vp-p
OUTPUT CHARACTERISTICS, RX DATA AND RX DATA
"1" State
IOH = -0.4 mA
VOH
2.5
3.6
-
V
"0" State
IOL = 4 mA
VOL
-
0.35
0.5
V
Receiver Output Skew
6/t
RXSK
-
-
10
nS
Delay (average), from differential input zero
crossings to RX DATA and RX DATA output
50% points
7/tDRX
-
300
450
nS
POWER SUPPLY CURRENTS PER CHANNEL 1/ 2/
VCC = +12V to +15V, VEE = -12V to -15V, VL = +5V
Duty Cycle
Condition
Symbol
Typ
Max
Unit
Transmitter Standby
Pt. B -B'
ZO = 70 Ω,
VO = 29 VPK-PK
Bit Pattern = FFFF
HEX
Figure 4
ICC
IEE
IL
5
25
18
10
35
30
mA
25%
ICC
IEE
IL
20
40
18
30
60
30
50%
ICC
IEE
IL
40
60
18
60
80
30
100%
ICC
IEE
IL
85
105
18
120
140
30



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