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UT63M-147CCA Folha de dados(PDF) 8 Page - Aeroflex Circuit Technology

Nome de Peças UT63M-147CCA
Descrição Electrónicos  MIL-STD-1553A/B Bus Transceiver
PDF  20 Pages
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Fabricante Electrônico  AEROFLEX [Aeroflex Circuit Technology]
Página de início  http://www.aeroflex.com
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UT63M-147CCA Folha de dados(HTML) 8 Page - Aeroflex Circuit Technology

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Appendix 2 - 8
ABSOLUTE MAXIMUM RATINGS 1
Notes:
1. Stress outside the listed absolute maximum rating may cause permanent damage to the devices. This is a stress rating only, and functional operation of the device
at these or any other conditions beyond limits indicated in the operational sections of this specification is not recommended. Exposure to absolute maximum
rating conditions for extended periods may affect device reliability.
2. Mounting per MIL-STD-883, Method 1012.
RECOMMENDED OPERATING CONDITIONS
PARAMETER
LIMITS
UNIT
VCC
-0.3 to +7.0
V
Input voltage range (receiver)
10
VPP, L-L
Logic input voltage range
-0.3 to +5.5
V
Power dissipation 100% duty cycle (per channel)
3.6
W
Thermal impedance junction to case2
6.0
°C/W
Maximum junction temperature
+175
°C
Storage temperature
-65 to +150
°C
Receiver common mode input voltage range
-5.0 to +5.0
V
PARAMETER
LIMITS
UNIT
Supply voltage range
+4.50 to +5.50
V
Logic input voltage range
0 to +5.0
V
Receiver differential voltage
8.0
VP-P
Receiver common mode voltage range
+4.0
V
Driver peak output current
600
mA
Serial data rate
0.3 to 1
MHz
Case operating temperature range (TC)
-55 to +125
°C
A
TERMINAL
Notes:
1. Transformer Coupled Stub:
Terminal is defined as transceiver plus isolation transformer. Point A is defined in figure 7.
2. Direct Coupled Stub:
Terminal is defined as transceiver plus isolation transformer and fault resistors. Point A is defined in figure 6.
RL
TXOUT
TXOUT
Figure 8. Transceiver Test Circuit MIL-STD-1553



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