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UT63M147CCC Datasheet(PDF) 10 Page - Aeroflex Circuit Technology

Part # UT63M147CCC
Description  MIL-STD-1553A/B Bus Transceiver
PDF  20 Pages
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Manufacturer  AEROFLEX [Aeroflex Circuit Technology]
Direct Link  http://www.aeroflex.com
Logo AEROFLEX - Aeroflex Circuit Technology

UT63M147CCC Datasheet(HTML) 10 Page - Aeroflex Circuit Technology

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Appendix 2 - 10
RECEIVER ELECTRICAL CHARACTERISTICS 1
VCC = 5.0V ±10%
-55
°C < T
C < +125°C
Notes:
1. All tests guaranteed per test figure 6.
2. Capacitance is measured only for initial qualification and after any process or design changes which may affect input or output capacitance.
3. Pass/fail criteria per the test method described in MIL-HDBK-1553 Appendix A, RT Validation Test Plan, Section 5.1.2.2, Common Mode Rejection.
4. Guaranteed by design.
5. Guaranteed to the limits specified if not tested.
SYMBOL
PARAMETER
MINIMUM
MAXIMUM
UNIT
CONDITION
CIN
2
Input capacitance
15
pF
RXEN; input
ƒ = 1MHz @ 0V
COUT
2
Output capacitance
20
pF
RXOUT, RXOUT;
ƒ = 1MHz @ 0V
VIC
5
Common mode input
voltage
-5
5
V
Direct-coupled stub; input 1.2 VPP,
200ns rise/fall time
±25ns,
ƒ = 1MHz
VTH
Input threshold
voltage4 (no response)
Input threshold voltage
(no response)
Input threshold
voltage4 (response)
Input threshold voltage
(response)
0.86
1.20
0.20
0.28
14.0
20.02
VPP,L-L
VPP,L-L
VPP,L-L
VPP,L-L
Transformer-coupled stub; input at
ƒ = 1MHz, rise/fall time 200ns at
(Receiver output 0
→ 1 transition)
Direct-coupled stub; input at
ƒ = 1MHz,
rise/fall time 200ns at (Receiver output
0
→ 1 transition)
Transformer-coupled stub; input at
ƒ = 1MHz, rise/fall time 200ns at
(Receiver output 0
→ 1 transition)
Direct-coupled stub; input at
ƒ = 1MHz,
rise/fall time 200ns at (Receiver output
0
→ 1 transition)
CMRR5
Common mode
rejection ratio
Pass/Fail 3
N/A



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