Typical Hybrid Power Dissipation
*
, Per Channel
Std Version
Power
Supply
Conditions
PSC1
V
CC
= +15V
V
EE
= -15V
V
L
= +5V
PSC2
V
CC
= +15V
V
EE
= -12V
V
L
= +5V
PSC3
V
CC
= +12V
V
EE
= -12V
V
L
= +5V
-L Version
Standby
100%
Duty
Cycle
Unit
Condition
Standby
Pt. B - B’
Z
O
= 70
Ω,
V
O
= 29 V
PK
-
PK
Bit Pattern = FFFF
HEX
Fig. 4
100%
Duty
Cycle
1.325
3.250
0.540
2.167
1.118
3.142
0.465
1.852
Watts
1.085
2.472
0.450
1.600
*
See Aeroflex Application note# 112 for reference.
Recommended Power Supply Voltage Range
+V
-V
Logic
+11.4 Volts to +15.75 Volts
-11.4 Volts to -15.75 Volts
+4.5 Volts to +5.5 Volts
Notes:
1. V
CC
= +15Volts ±0.75V, V
EE
= -15Volts ±0.75V, V
IL
= +5Volts ±0.5V, T
C
= -55°C to +125°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 4, in accordance with MIL-STD-1553B
paragraph 4.5.2.2.2.3.
5. At point A-A’ on Figure 3 or 4, 2.5 µS after midpoint crossing of the parity bit of the last word of a 660 µS message.
6. Receiver skew is defined as the time from the rising edge of RX DATA OUT to the rising edge of RX DATA OUT
minus 500 nS, with a sine wave input of 3 V
PK
-
PK
at 1MHz driven into Pt. B-B’ of Figure 4 or 2.1 V
PK
-
PK
at 1MHz
driven into Pt. B-B’ of Figure 3. The specification maximum is guaranteed for T
A
= 25°C only. Standard TTL loads
applied to RX DATA Outputs.
7. 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.
Aeroflex Circuit Technology
5
SCD4808 REV E 12/9/99
Plainview NY (516) 694-6700
AEROFLEX [ AEROFLEX CIRCUIT TECHNOLOGY ]
