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ACT4444 Datasheet(PDF) 5 Page - Aeroflex Circuit Technology

Part # ACT4444
Description  Transceiver for MIL-STD-1553 /MACAIR in a Chipscale Package
PDF  10 Pages
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Manufacturer  AEROFLEX [Aeroflex Circuit Technology]
Direct Link  http://www.aeroflex.com
Logo AEROFLEX - Aeroflex Circuit Technology

ACT4444 Datasheet(HTML) 5 Page - Aeroflex Circuit Technology

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SCD4444 Rev B
TYPICAL HYBRID POWER DISSIPATION
*
Power Supply
Conditions
Condition
Standby
100% Duty
Cycle
Unit
PSC1
VCC = +15V
VEE = -15V
VL = +5V
Pt. B - B’, ZO = 70 Ω, VO = 29 VPK-PK
Bit Pattern = FFFF
HEX
Figure 3 or 4
0.540
2.167
Watts
PSC2
VCC = +15V
VEE = -12V
VL = +5V
0.465
1.852
PSC3
VCC = +12V
VEE = -12V
VL = +5V
0.450
1.600
* See Aeroflex Application note# 112 for reference.
RECOMMENDED POWER SUPPLY VOLTAGE RANGE
VCC
+11.4 Volts to +15.75 Volts
VEE
-11.4 Volts to -15.75 Volts
VL
+4.5 Volts to +5.5 Volts
Notes:
1. VCC = +15Volts ±0.75V, VEE = -15Volts ±0.75V, VIL = +5Volts ±0.5V, TC = -40°C to +85°C, unless otherwise specified.
2. All typical values are measured at +25°C.
3. Characteristics guaranteed by design, not production tested.
4. Power ON/OFF, measured from 75KHz to 1MHz at Point A-A’ Figure 3 or 4, in accordance with MIL-STD-1553B paragraph
4.5.2.2.2.3.
5. At point A-A’ on Figure 3 or 4, 2.5µS after midpoint crossing of the parity bit of the last word of a 660 µS message.
6. This test is peformed while the Transceiver is reading its own transmission. This condition is called "Wraparound". Standard TTL
loads applied to RX DATA Outputs.



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