UT54ACTS20E - Aeroflex Microelectronic Solutions

UT54ACTS20E
Dual 4-Input NAND Gates
December 2014
www.aeroflex.com/Logic
Advanced Datasheet
FEATURES
.
• 0.6μm CRH CMOS Process
•
•
•
•
•
•
- Latchup immune
High speed
PINOUT
14-Lead Flatpack
Top View
Low power consumption
Wide power supply operating range of 3.0V to 5.5V
Available QML Q or V processes
A1
1
14
14-lead flatpack
B1
VDD
2
13
D2
UT54ACTS20E - SMD 5962-96527
NC
3
12
C2
C1
4
11
D1
5
10
NC
B2
Y1
6
9
A2
VSS
7
8
Y2
DESCRIPTION
The UT54ACTS20E are dual 4-input NAND gates. The circuits
perform the Boolean functions Y = A⋅B⋅C⋅D or Y = A+B+C+D
in positive logic.
The device is characterized over full military temperature range
of -55°C to +125°C.
LOGIC DIAGRAM
FUNCTION TABLE
OUTPUT
INPUTS
A
B
C
D
Y
H
H
H
H
L
L
X
X
X
H
X
L
X
X
H
X
X
L
X
H
X
X
X
L
H
LOGIC SYMBOL
A1
B1
C1
D1
A2
B2
C2
D2
(1)
(2)
(4)
A1
B1
C1
D1
Y1
A2
B2
C2
D2
Y2
&
(6)
(5)
Y1
(9)
(10)
(12)
(13)
(8)
Y2
Note:
1. Logic symbol in accordance with ANSI/IEEE standard 91-1984 and IEC
Publication 617-12.
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OPERATIONAL ENVIRONMENT 1
PARAMETER
LIMIT
UNITS
Total Dose
1.0E6
rads(Si)
SEU Threshold 2
108
MeV-cm2/mg
SEL Threshold
120
MeV-cm2/mg
Neutron Fluence
1.0E14
n/cm2
Notes:
1. Logic will not latchup during radiation exposure within the limits defined in the table.
2. Device storage elements are immune to SEU affects.
ABSOLUTE MAXIMUM RATINGS
SYMBOL
PARAMETER
LIMIT
UNITS
VDD
Supply voltage
-0.3 to 7.0
V
VI/O
Voltage any pin
-0.3 to VDD + 0.3
V
TSTG
Storage Temperature range
-65 to +150
°C
TJ
Maximum junction temperature
+175
°C
TLS
Lead temperature (soldering 5 seconds)
+300
°C
ΘJC
Thermal resistance junction to case
15.5
°C/W
II
DC input current
±10
mA
PD2
Maximum package power dissipation
3.2
W
o
permitted @ Tc = +125 C
Note:
1. Stresses outside the listed absolute maximum ratings may cause permanent damage to the device. This is a stress rating only, functional operation of the device at these
or any other conditions beyond limits indicated in the operational sections is not recommended. Exposure to absolute maximum rating conditions for extended periods
may affect device reliability.
2. Per MIL-STD-883, method 1012.1, Section 3.4.1, PD = (Tj(max) - Tc(max) ) / Θjc
RECOMMENDED OPERATING CONDITIONS
SYMBOL
PARAMETER
LIMIT
UNITS
VDD
Supply voltage
3.0 to 5.5
V
VIN
Input voltage any pin
0 to VDD
V
TC
Temperature range
-55 to +125
°C
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DC ELECTRICAL CHARACTERISTICS FOR THE UT54ACTS20E7
( VDD = 3.0V to 5.5V; VSS = 0V6; -55°C < TC < +125°C)
SYMBOL
DESCRIPTION
CONDITION
MIN
MAX
UNIT
VIL1
Low-level input voltage 1
VDD from 4.5V to 5.5V
0.8
V
VIL2
Low-level input voltage 1
VDD from 3.0V to 3.6V
0.8
V
VIH1
High-level input voltage 1
VDD from 4.5V to 5.5V
0.5 VDD
V
VIH2
High-level input voltage 1
VDD from 3.0V to 3.6V
2.0
V
Input leakage current
VIN = VDD or VSS
-1
Low-level output voltage 3
IOL = 8mA
IIN
VOL1
1
μA
0.4
V
0.4
V
VDD = 4.5V to 5.5V
VOL2
Low-level output voltage 3
IOL = 6mA
VDD = 3.0V to 3.6V
VOH1
High-level output voltage 3
IOH = -8mA
0.7 VDD
V
2.4
V
VDD from 4.5V to 5.5V
VOH2
High-level output voltage 3
IOH = -6mA
VDD from 3.0V to 3.6V
IOS1
Short-circuit output current 2 ,4
VO = VDD and VSS
-200
+200
mA
-100
+100
mA
VDD from 4.5V to 5.5V
IOS2
Short-circuit output current 2 ,4
VO = VDD and VSS
VDD from 3.0V to 3.6V
IOL1
Low level output current 10
VIN = VDD or VSS
+8
mA
+6
mA
-8
mA
VOL = 0.4V
VDD from 4.5V to 5.5V
IOL2
Low level output current 10
VIN = VDD or VSS
VOL = 0.4V
VDD from 3.0V to 3.6V
IOH1
High level output current 10
VIN = VDD or VSS
VOH = VDD-0.4V
VDD from 4.5V to 5.5V
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IOH2
High level output current10
VIN = VDD or VSS
-6
mA
VOH = VDD-0.4V
VDD from 3.0V to 3.6V
Ptotal1
Power dissipation 2, 8, 9
CL = 50pF
1.1
mW/
MHz
0.5
mW/
MHz
25
μA
1.6
mA
15
pF
15
pF
VDD = 4.5V to 5.5V
Ptotal2
Power dissipation 2, 8, 9
CL = 50pF
VDD = 3.0V to 3.6V
IDDQ
Quiescent Supply Current
VIN = VDD or VSS
VDD from 3.6V to 5.5V
ΔIDDQ
Quiescent Supply Current Delta
For input under test
VIN = VDD - 2.1V
For all other inputs
VIN = VDD or VSS
VDD = 5.5V
CIN
Input capacitance 5
ƒ = 1MHz
VDD = 0V
COUT
Output capacitance 5
ƒ = 1MHz
VDD = 0V
Notes:
1. Functional tests are conducted in accordance with MIL-STD-883 with the following input test conditions: VIH = VIH(min) + 20%, - 0%; VIL = VIL(max) + 0%, 50%, as specified herein, for TTL, CMOS, or Schmitt compatible inputs. Devices may be tested using any input voltage within the above specified range, but are
guaranteed to VIH(min) and VIL(max).
2. Supplied as a design limit but not guaranteed or tested.
3. Per MIL-PRF-38535, for current density ≤5.0E5 amps/cm2, the maximum product of load capacitance (per output buffer) times frequency should not exceed 3,765pF/
MHz.
4. Not more than one output may be shorted at a time for maximum duration of one second.
5. Capacitance measured for initial qualification and when design changes may affect the value. Capacitance is measured between the designated terminal and VSS at
frequency of 1MHz and a signal amplitude of 50mV rms maximum.
6. Maximum allowable relative shift equals 50mV.
7.For devices procured with a total ionizing dose tolerance guarantee, the post-irradiation performance is guaranteed at 25°C per MIL-STD-883, method 1019, condition
A up to the maximum TID level producred.
8. Power dissipation specified per switching output.
9. Power does not include power contribution of any TTL output sink current.
10. Guaranteed by characterization, but is not tested.
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AC ELECTRICAL CHARACTERISTICS FOR THE UT54ACTS20E2
(VDD = 3.0V to 5.5V; VSS = 0V 1, -55°C < TC < +125°C);
SYMBOL
PARAMETER
CONDITION
VDD
tPLH
Input to Yn
CL = 50pF
4.5V to 5.5V
tPHL
Input to Yn
CL = 50pF
MINIMUM
MAXIMUM
UNIT
1
6
ns
3.0V to 3.6V
1
9.5
4.5V to 5.5V
1
7.5
3.0V to 3.6V
1
10.5
ns
Notes:
1. Maximum allowable relative shift equals 50mV.
2. For devices procured with a total ionizing dose tolerance guarantee, the post-irradiation performance is guaranteed at 25°C per MIL-STD-883, method 1019, condition
A up to the maximum TID level producred.
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Packaging
1. All exposed metallized areas are gold plated over
electroplated nickel per MIL-PRF-38535.
2. The lid is electrically connected to VSS.
3. Lead finishes are in accordance with MIL-PRF38535.
4. Dimension symbol is in accordance with MILPRF-38533.
5. Lead position and colanarity are not measured.
Figure 1. 14-lead Flatpack
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Ordering Information: UT54ACTS20E: SMD
5962 * ***** ** * * *
Lead Finish: (Notes 1 & 2)
A = Solder
C = Gold
X = Optional
Package Type:
X = 14-lead ceramic bottom-brazed dual-in-line Flatpack
Class Designator:
Q = QML Class Q
V = QML Class V
Device Type:
02 = 1 rad(Si)/sec
03 = 50 to 300 rads(Si)/sec
Drawing Number:
96527 = UT54ACTS20E
Total Dose: (Notes 3 & 4)
R = 1E5 rads(Si)
F = 3E5 rads(Si)
G = 5E5 rads(Si)
H = 1E6 rads(Si)
Notes:
1. Lead finish (A,C, or X) must be specified.
2. If an “X” is specified when ordering, part marking will match the lead finish and will be either “A” (solder) or “C” (gold).
3. Total dose radiation must be specified when ordering. QML Q and QML V not available without radiation hardening. For prototype inquiries, contact factory.
4. Device type 02 is only offered with a TID tolerance guarantee of 3E5 rads(Si) or 1E6 rads(Si) and is tested in accordance with MIL-STD-883 Test Method 1019
Condition A and section 3.11.2. Device type 03 is only offered with a TID tolerance guarantee of 1E5 rads(Si), 3E5 rads(Si), and 5E5 rads(Si), and is tested in
accordance with MIL-STD-883 Test Method 1019 Condition A.
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Aeroflex Colorado Springs - Datasheet Definition
Advanced Datasheet - Product In Development
Preliminary Datasheet - Shipping Prototype
Datasheet - Shipping QML & Reduced HiRel
This product is controlled for export under the U.S. Department of Commerce (DoC). A license may
be required prior to the export of this product from the United States.
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[email protected]
Aeroflex Colorado Springs (Aeroflex) reserves the right to
make changes to any products and services herein at any time
without notice. Consult Aeroflex or an authorized sales
representative to verify that the information in this data sheet
is current before using this product. Aeroflex does not assume
any responsibility or liability arising out of the application or
use of any product or service described herein, except as
expressly agreed to in writing by Aeroflex; nor does the
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convey a license under any patent rights, copyrights,
trademark rights, or any other of the intellectual rights of
Aeroflex or of third parties.
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Datasheet Revision History
Revision Date
December 2014
Version 1.0.0
36-00-04-003
Ver. 1.0.0
Description of Change
Initial Release of Data Sheet
9
Aeroflex Microelectronics Solutions - HiRel