SSC SS6845G

SS6845G
Regulated 5V Charge Pump
DESCRIPTION
PRODUCT SUMMARY
Input voltage range: 2.7V to 5.0V
Regulated output voltage of 5V ±4%
Output current: 100mA (VIN = 3.3V)
110mA (VIN = 3.6V)
The SS6845G is a micropower charge pump
DC/DC converter that produces a regulated 5V
output. The input voltage range is 2.7V to 5.0V.
Extremely low operating current (13µA typical
with no load) and a low external part count (one
FEATURES
0.22µF flying capacitor and two small bypass
Ultralow power: I IN = 13µA
No inductors needed
capacitors at the input and output) make the
Very low shutdown current: <1µA
Internal oscillator: 650KHz
Short-circuit and over-temperature protection
SS6845G ideally suitable for small, batterypowered applications.
The SS6845G operates as a PSM-mode
(Pulse Skipping Modulation) switched capacitor
APPLICATIONS
voltage doubler to produce a regulated output
and features thermal shutdown capability and
White or Blue LED Backlighting
SIM Interface Supplies for Cellular Telephones
Li-Ion Battery Backup Supplies
Local 3V to 5V Conversion
Smart Card Readers
PCMCIA Local 5V Supplies
short circuit protection.
Pb-free; RoHS-compliant SOT-23-6 package
TYPICAL APPLICATION CIRCUIT
VOUT
** R1
U1
1-Cell
1 VOUT
CIN
2.2µF
Li-ion Battery
2
GND
C+ 6
VIN
3
SHDN
C-
COUT
2.2µF
*
*
*
*
5
4
0.22µF
CFLY
SS6845G
Regulated 5V Output from 2.7V to 5.0V Input
*
WLED series number: NSPW310BS, VF=3.6V, IF=20mA
**
R1 =
VOUT − VF
, where NWLED is the number of WLEDs.
IF × N WLED
CIN, COUT: CELMK212BJ225MG (X5R) (0805), TAIYO YUDEN
CFLY
7/21/2005 Rev.3.01
: CEEMK212BJ224KG (X7R) (0805), TAIYO YUDEN
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SS6845G
ORDERING INFORMATION
PIN CONFIGURATION
SS6845GG TR
Packing type:
TR: Tape and reel
SOT-23-6
TOP VIEW
C+ VIN
6
5
C4
(MARK SIDE)
Package type:
GG: RoHS-compliant SOT-23-6
1
2
3
VOUT GND SHDN
SOT-23-6 Marking
Part No.
Marking
SS6845GG
BO50P
ABSOLUTE MAXIMUM RATINGS
VIN to GND
6V
VOUT to GND
6V
All other ins to GND
6V
VOUT short-circuit duration
Continuous
Operating ambient temperature range
Junction temperature
-40°C to 85 °C
125°C
-65°C to 150 °C
Storage temperature range
Lead temperature (minimum 10 seconds)
260°C
Absolute Maximum Ratings are those values beyond which the life of a device may be impaired.
TEST CIRCUIT
Refer to the TYPICAL APPLICATION CIRCUIT on page 1.
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SS6845G
ELECTRICAL CHARACTERISTICS
(TA=25°C, CFLY=0.22µF, CIN=2.2µF, COUT=2.2µF, unless otherwise specified.) (Note 1)
PARAMETER
TEST CONDITIONS
Input voltage
Output voltage
Continuous output current
Supply current
Shutdown current
Output ripple
Efficiency
Switching frequency
Shutdown input threshold
(High)
Shutdown input threshold
(Low)
Shutdown input current
(High)
Shutdown input current
(Low)
2.7V≤ VIN< 3.3V,
IOUT≤ 30mA
3.3V≤ VIN≤ 5.0V,
IOUT≤ 60mA
VIN=3V, VOUT=5.0V
SHDN =VIN
2.7V≤ VIN≤ 5.0V,
IOUT=0 , SHDN =VIN
2.7V≤ VIN≤ 5.0V,
IOUT=0 , SHDN =0V
VIN =3V, IOUT=50mA
VIN =2.7V , IOUT=30mA
Oscillator free-running
SYMBOL
MIN.
VIN
2.7
4.8
TYP.
5.0
MAX.
UNIT
5.0
V
5.2
VOUT
V
4.8
IOUT
5.0
5.2
60
mA
ICC
13
30
µA
I SHDN
0.01
1.0
µA
VR
60
mV
η
83
%
fOSC
650
KHz
VIH
1.4
V
VIL
0.3
V
SHDN =VIN
IIH
-1
1
µA
SHDN = 0V
IIL
-1
1
µA
Vout turn-on time
VIN =3V, IOUT = 0mA
tON
0.5
mS
Output short-circuit current
VIN=3V, VOUT= 0V,
SHDN = VIN
ISC
170
mA
Note1: Specifications are production tested at TA=25°C. Specifications over the -40°C to 85°C operating
temperature range are assured by design, characterization and correlation with Statistical Quality
Controls (SQC).
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SS6845G
TYPICAL PERFORMANCE CHARACTERISTICS
(CN, COUT: CELMK212BJ225MG, CFLY: CEEMK212BJ224KG)
5.15
20
IOUT=25mA
COUT=10µF
CFLY=1µF
5.05
Supply Current (µΑ)
Output Voltage (V)
5.10
TA = -40°C
5.00
4.95
TA =25°C
4.90
TA=-40°C
15
10
IOUT=0µA
CFLY=1µF
VSHDN=VIN
TA =85°C
4.85
2.5
3.0
3.5
4.0
4.5
5
5.0
2.5
3.0
3.5
Supply Voltage (V)
5.1
5.05
Output Voltage (V)
Output Voltage (V)
5.0
5.2
TA=25°C
COUT=10µF
CFLY=1µF
5.10
VIN=3.6V
5.00
4.95
5.0
4.9
4.8
VIN=3.3V VIN=3.6V
4.7
TA=25°C
CFLY=0.22µF
COUT=2.2µF
VIN=3.3V
4.90
VIN=2.7V
4.85
0
20
4.6
VIN=3.0V
40
60
80
100
120
140
4.5
160
0
10
20
30
VIN=2.7V
40
50
60
70
VIN=3.0V
80
90 100 110 120 130
Output Current (mA)
Output Current (mA)
Fig. 4 Load Regulation
Fig. 3 Load Regulation
100
100
CT=25°C
CFLY=1µF
VIN=2.7V
90
70
60
VIN=3.0V
50
VIN=3.3V
40
VIN=3.6V
Efficiency (%)
Efficiency (%)
4.5
Fig. 2 No Load Supply Current vs. Supply Voltage
5.15
80
4.0
Supply Voltage (V)
Fig. 1 Line Regulation
90
TA=85°C
TA=25°C
VIN=2.7V
VIN=3.0V
80
70
60
50
30
20
TA=25°C
CFLY=0.22µF
40
10
0
0.001
0.01
0.1
1
10
100
30
0.01
Output Current (mA)
0.1
1
10
100
Output Current (mA)
Fig. 6 Efficiency
Fig. 5 Efficiency
7/21/2005 Rev.3.01
VIN=3.6V
VIN=3.3V
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SS6845G
TYPICAL PERFORMANCE CHARACTERISTICS (Continued)
50
175
45
150
35
Output Ripple (mV)
Output Ripple (mV)
40
VIN=3.6V
30
25
VIN=3.3V
20
15
VIN=3.0V
10
0
COUT=10µF
VIN=2.7V
5
0
20
40
60
100
120
VIN=3.6V
100
75
VIN=3.3V
50
VIN=2.7V
CFLY=0.22µF
0
140
0
20
40
Fig.7 Output Current vs. Output Ripple
60
80
100
120
Output Current (mA)
Output Current (mA)
140
Fig. 8 Output Current vs. Output Ripple
1000
5.05
VIN=2.5V
Output Voltage (V)
900
Frequency (KHz)
COUT=2.2µF
VIN=3.0V
25
CFLY=1µF
80
125
800
700
600
5.00
VIN=3.0V
CFLY=1µF
IOUT=50mA
4.95
4.90
500
400
-60
-40
-20
0
20
40
60
80
100
120
4.85
-60
140
Temperature (°C)
Fig. 9 Frequency vs. Temperature
-40
-20
Fig. 10
0
20
40
60
80
100
120
140
Temperature (°C)
Output Voltage vs. Temperature
220
TA=25°C
CFLY=1µF
260
240
Short-Circuit Current (mA)
Short-Circuit Current (mA)
280
220
200
180
160
140
120
100
200
180
160
140
120
TA=25°C
CFLY=0.22µF
100
2.5
3.0
3.5
4.0
4.5
5.0
2.5
Supply Voltage (V)
3.5
4.0
4.5
5.0
5.5
Supply Voltage (V)
Fig. 11 Short-Circuit Current vs. Supply Voltage
7/21/2005 Rev.3.01
3.0
Fig. 12 Short-Circuit Current vs. Supply Voltage
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SS6845G
TYPICAL PERFORMANCE CHARACTERISTICS (Continued)
CN
CN
VOUT
VOUT
Fig. 13
Output Ripple
VIN=3.0V, IOUT=50mA, COUT=10µF,CFLY=1µF
Fig. 14 Output Ripple
VIN=3.0V, IOUT=50mA, COUT=2.2µF, CFLY=0.22µF
VOUT
IOUT
VOUT
Fig. 15 Load Transient Response
VIN=3.0V, IOUT=0mA~50mA,COUT=10µF, CFLY=1µF
IOUT
Fig. 16 Load Transient Response
VIN=3.0V, IOUT=0mA~50mA,COUT=2.2µF, CFY=0.22µF
VOUT
V SHDN
Fig. 17 Start-Up Time
VIN=3.0V, IOUT=0A, COUT=10µF
7/21/2005 Rev.3.01
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VOUT
V SHDN
Fig. 18 Start-Up Time
VIN=3.0V, IOUT=0A, COUT=2.2µF
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SS6845G
BLOCK DIAGRAM
VOUT
2
COUT
2.2µF
C+
1
VIN
CFLY
2
Control
0.22µF
CIN
2.2µF
COMP
CVREF
SHDN
1
PIN DESCRIPTIONS
PIN 1:VOUT -
PIN 2: GND -
Regulated output voltage. For the
best performance, VOUT should be
bypassed with a 2.2µF (min) low
ESR capacitor with the shortest
possible leads.
PIN 4: C-
-
Flying capacitor negative terminal.
PIN 5: VIN
-
Input supply voltage. VIN should
be bypassed with a 2.2µF (min)
low ESR capacitor.
Ground. Should be tied to a
ground plane for best performance.
PIN 6: C+
-
Flying capacitor positive terminal.
PIN 3: SHDN - Active-low shutdown input. A low
voltage on SHDN disables the
SS6845G. SHDN is not allowed to
float.
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SS6845G
APPLICATION INFORMATION
Introduction
Short Circuit/Thermal Protection
The SS6845G is a micropower charge pump DC/DC
The SS6845G includes built-in short circuit current
converter that produces a regulated 5V output
limiting as well as over-temperature protection.
with an input voltage range from 2.7V to 5.0V. It
During a short circuit condition, the output current
utilizes the charge pump topology to boost VIN to
a regulated output voltage. Regulation is obtained
is automatically constrained to approximately
by sensing the output voltage through an internal
in the internal IC junction temperature. When the
resistor divider. A switched doubling circuit
die temperature exceeds 150°C, the thermal
enables the charge pump when the feedback
protection will shut down the charge pump switching
voltage is lower than the trip point of the internal
operation and the die temperature will then
comparator, and vice versa. When the charge
reduce. Once the die temperature drops below
pump is enabled, a two-phase non-overlapping
135°C, the charge pump switching circuit will
clock activates the charge pump switches. To
restart. If the fault has not been eliminated, the
maximize battery life for a battery-use application,
this protection mechanism will repeat again and
quiescent current is limited to no more than 13µA.
again, allowing the SS6845G to work continuously
170mA. This short circuit current will cause a rise
in a short circuit condition without damaging the
Operation
device.
This kind of converter uses capacitors to store
and transfer energy. Since the capacitors can’t
change their voltage level abruptly, the voltage
Shutdown
ratio of VOUT over VIN is limited to some range.
Capacitive voltage conversion is obtained by
In shutdown mode, the output is disconnected
switching a capacitor periodically. It first charges
since most of the circuitry is turned off. Due to
the capacitor by connecting it across a voltage
high impedance, the shutdown pin cannot float.
from the input. The input current is extremely low
source and then connects it to the output.
Referring to Fig. 19, during the on state of internal
clock, Q1 and Q4 are closed, which charges C1 to
VIN level. During the off state, Q3 and Q2 are
closed. The output voltage is VIN plus VC1, that is,
2VIN.
VIN
Q2 VOUT
Q1
CIN
COUT
C1
Q3
Q4
Fig. 19 The circuit of charge pump
Efficiency
The diagrams, Fig. 20 and Fig. 21 show the operation
of the charge pump in the on and off states.
R DS-ON is the resistance of the switching element
during conduction. ESR is the equivalent series
resistance of the flying capacitor C1. ION-AVE and
IOFF-AVE are the average current during the on-state
and off-state, respectively. D is the duty-cycle, which
means the ratio of the on-state time to the total cycle
time. Let's look at capacitor C 1 - assuming that
capacitor C 1, has reached its steady state, then the
amount of charge flowing into C 1 during the on-state
is equal to that flowing out of C 1 during the off-state.
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SS6845G
ION− AVE × DT = IOFF − AVE × (1 − D)T
(1)
External Capacitor Selection
ION- AVE × D = IOFF - AVE × (1 − D)
(2)
Three external capacitors, CIN, COUT and CFLY,
determine SS6845G performance, in the area of
IIN = ION- AVE × D + IOFF- AVE × (1 − D)
= 2 × ION- AVE × D
(3)
= 2 × IOFF- AVE × (1 - D)
output ripple voltage, charge pump strength and
transients. Optimum performance can be obtained
by the use of ceramic capacitors with low ESR.
Due to their high ESR, tantalum and aluminum
IOUT = IOFF- AVE × (1 − D)
..........(4)
IIN = 2IOUT
capacitors are not recommended for charge-pump
applications.
For the SS6845G, the controller uses the PSM
(Pulse Skipping Modulation) control strategy. When
To reduce noise and ripple, a low ESR ceramic
the duty cycle is limited to 0.5, then:
capacitor, ranging from 2.2µF to 10µF, is
ION- AVE × 0.5 × T = IOFF- AVE × (1 − 0.5) × T
ION- AVE = IOFF- AVE
..........(5)
According to the equation (4), we know that as
long as the flying capacitor C1 is at steady state,
the input current is twice the output current. The
efficiency of charge pump is given below:
η =
VIN
VOUT × IOUT
V
×I
V
= OUT OUT = OUT ..(6)
VIN × IIN
VIN × 2IOUT
2VIN
ION
Q2
Q1
RDS-ON
CIN
Q3
COUT
ESR
C1
VOUT
recommended for CIN and COUT. The value of
COUT determines the amount of output ripple
voltage. An output capacitor with a larger value
results in smaller ripple.
CFLY is critical to the performance of a charge pump.
The larger CFLY is, the larger the output current and
the smaller the resulting ripple voltage. However,
a large CFLY requires large CIN and COUT.
The ratio of CIN (as well as COUT) to CFLY should
be approximately 10:1.
The values of the capacitors used under operating
conditions, determine the performance of the charge
Q4
pump converter, and two factors, described below,
affect the value of the capacitors.
RDS-ON
Fig. 20 The on-state of charge pump circuit
1. Material: Ceramic capacitors of different
materials, such as X7R, X5R, Z5U and Y5V,
VIN
CIN
RDS-ON
Q2
Q1
Q3
VOUT
COUT
ESR
capacitance can vary significantly. For example,
X7R or X5R types of capacitor retain their
capacitance over temperatures from -40°C
Q4
RDS-ON
have different tolerances to temperature and
to 85°C, but a Z5U or Y5V type will change a
C1
lot over that temperature range.
IOFF
Fig. 21 The off-state of charge pump circuit
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SS6845G
2. Package Size: A ceramic capacitor with
large volume (0805), gets a lower ESR than
a small one (0603). Therefore, larger devices
With a duty-cycle of 0.5, the power loss of RDS-ON is
2
×
PRDS −ON ≅ IOUT
provide improved transient response over
2
× RDS - ON
0.5(1 − 0.5)
2
= IOUT
× 8R DS − ON
smaller ones.
Table 1 lists the recommended components for
2
PESR ≅ IOUT
× ESR ×
use with the SS6845G.
2
= IOUT
× 4ESR
Table.1 Bill of Material
Design-
Part
ator
Type
CIN
2.2µ
CFLY
0.22µ
COUT
2.2µ
1
0.5(1 − 0.5)
Description
Vendor
CELMK212BJ-
TAIYO
225MG (X5R)
YUDEN
In fact, whether the current is the on-state or the
off-state, it decays exponentially rather than flows
CEEMK212BJ
TAIYO
-224KG (X7R)
YUDEN
CELMK212BJ-
TAIYO
225MG (X5R)
YUDEN
steadily, and as the root mean square value of
exponential decay is not equal to that of steady
flow, then we must use an approximation.
Let’s use another approach to look at the charge
pump circuit and focus on the flying capacitor
C1. Referring to Fig. 20, when the circuit is in the
Power Dissipation
on state, the voltage across C1 is:
Now, let’s look at the power dissipation in R DS-ON
VC-ON (t) = VIN − 2R DS−ON × ION (t) - ESR × ION (t) …(9)
and ESR. Assume that the RDS-ON of each internal
switching element in the SS6845G is equal and ESR
is the equivalent series resistance of CFLY (refer
to Fig. 20 and Fig. 21). The approximation of the
power losses of R DS-ON and ESR are given below:
PRDS−ON
2
≅ ION
- AVE
2
× 2RDS − ON × D + IOFF
- AVE
× 2RDS − ON × (1 − D)
IIN 2
I
) × 2RDS - ON × D + ( OUT )2 × 2RDS - ON × (1 - D)
2D
1- D
2IOUT 2
I
=(
) × 2RDS -ON × D + ( OUT )2 × 2RDS -ON × (1 - D)
2D
1- D
2
2
2
2
= IOUT
× ( RDS - ON ) + IOUT
×(
RDS -ON )
D
1- D
2
2
= IOUT
×
× RDS -ON
D(1 - D)
=(
..........(7)
2
2
PESR ≅ ION
− AVE × ESR × D + I OFF − AVE × ESR × (1 − D)
I
IIN 2
) × ESR × D + ( OUT ) 2 × ESR × (1 − D)
2D
1− D
1 2
1
2
= IOUT × ESR × + IOUT × ESR ×
D
1- D
1
2
= IOUT × ESR ×
D(1 - D)
=(
7/21/2005 Rev.3.01
The average of VC1 during the on-state is:
VC−ON− AVE = VIN − 2R DS−ON × ION− AVE − ESR × ION− AVE
……………………….(10)
Similarly, referring to Fig. 21, when the circuit is
in the off-state, the voltage of C1 is:
VC-OFF (t) =
VOUT − VIN + 2R DS-ON × IOFF (t) + ESR × IOFF (t)
……………………………(11)
The average of VC1 during the off-state is:
VC−OFF− AVE =
VOUT − VIN + 2R DS−ON × IOFF− AVE + ESR × IOFF− AVE
………………..(12)
The difference in charge stored in C 1 between the
on-state and off-state is the net charge transferred to
the output in one cycle.
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SS6845G
∆Q = Q ON - Q OFF
= C1 × (VC1−ON− AVE − VC1−OFF − AVE )
= C1 × (2VIN - VOUT - 2R DS-ON × ION- AVE - 2R DS-ON × IOFF- AVE - ESR × ION− AVE - ESR × IOFF- AVE )
………(13)
I
I
I
IOUT
− 2R DS −ON × OUT - ESR × OUT - ESR × OUT )
1- D
D
1− D
D
1
+ ESR) × IOUT ×
]
D(1 − D)
= C1 × (2VIN − VOUT − 2R DS −ON ×
= C1 × [2VIN − VOUT − (2R DS−ON
Thus the output current can be written as
IOUT = f × ∆Q = f × (Q ON − Q OFF )
= f × C1 × [2VIN − VOUT - (2R DS-ON + ESR ) × IOUT ×
(14)
1
]
D(1 - D)
When the duty cycle is 0.5, the output current can be written as:
IOUT = f × C1 × [2VIN − VOUT − (2R DS−ON + ESR) × IOUT ×
1
]
0.5(1 − 0.5)
(15)
= fC1 × [2VIN − VOUT − (8R DS−ON + 4ESR) × IOUT ]
And equation (15) can be re-written as:
2VIN − VOUT =
1
× IOUT + (8R DS−ON + 4ESR) × IOUT
fC1
According to equation (16), when the duty cycle
is 0.5, the equivalent circuit of the charge pump is
shown in Fig. 22. The term 8RDS-ON is the total
(16)
IOUT
2VIN
1/fC1
8RDS-ON
VOUT
4ESR
COUT
effect of switching resistance, 1/fC1 is the effect
LOAD
of flying capacitor and 4ESR is its equivalent
resistance.
Fig. 22 The equivalent circuit of charge pump
From the equivalent circuit shown in Fig. 22, it is
Layout Considerations
seen that the terms 1/fC1, 4ESR and 8RDS-ON
should be as small as possible to get large output
With the high switching frequency and transient
current. However, since the R DS-ON is internal to
currents of the SS6845G, careful consideration of
the SS6845G, all that can be done is to lower the
PCB layout is important. To achieve the best
values of 1/fC1 and ESR. However even if the
performance, it is necessary to minimize the distance
values of 1/fC1 and ESR can be kept as small as
between every component and also to minimize
possible, the term 8RDS-ON still dominates the
the length of every connection and maximize the
limit of the maximum output current.
trace width. Make sure each device connects to an
immediate ground plane. Fig. 23 to Fig. 25 show
a recommended layout.
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SS6845G
SS6845G
Fig. 23 Top layer
Fig. 24 Bottom layer
Fig. 25 Topover layer
APPLICATION EXAMPLES
VIN
CIN
2.2µ
1
2
3
VOUT
GND
VIN
SHDN
U1
2 GND
CAP+
VIN
3 SHDN
U2
CAP-
6
CFLY1
5
VOUT
COUT
2.2µF
0.22µF
4
SS6845G
1 VOUT
VSHDN
CAP+
CAP-
6
CFLY2
0.22µF
5
4
SS6845G
CIN, COUT : TAIYO YUDEN Ceramic Capacitor, CELMK212BJ225MG (X5R) (0805)
CFLY1, CFLY2: TAIYO YUDEN Ceramic Capacitor, CEEMK212BJ224KG (X7R) (0805)
Fig. 26 Using two SS6845G in parallel to provide larger output current.
USB
CIN
2.2µF
VOUT
1
2
3
VSHDN
VOUT
GND
SHDN
U1
CAP+
VIN
CAP-
6
5
4
COUT
2.2µF
CFLY
0.22µF
SS6845G
CIN, COUT: TAIYO YUDEN Ceramic Capacitor, CELMK212BJ225MG (X5R) (0805)
: TAIYO YUDEN Ceramic Capacitor, CEEMK212BJ224KG (X7R) (0805)
CFLY1
Fig. 27 Regulated 5V from USB
7/21/2005 Rev.3.01
www.SiliconStandard.com
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SS6845G
PHYSICAL DIMENSIONS
(unit: mm)
D
A
A
e
e1
SEE VIEW B
b
WITH PLATING
c
A
A2
SOT-23-6
MILLIMETERS
MIN.
MAX.
A
0.95
1.45
A1
0.05
0.15
A2
0.90
1.30
b
0.30
0.50
c
0.08
0.22
D
2.80
3.00
E
2.60
3.00
E1
1.50
1.70
E
E1
S
Y
M
B
O
L
0.95 BSC
1.90 BSC
L
0.30
L1
θ
0.60
0.60 REF
0°
8°
0.25
A1
BASE METAL
SECTION A-A
e
e1
GAUGE PLANE
SEATING PLANE
θ
L
L1
VIEW B
PART MARKING
PART NUMBER CODE: BO50P = SS6845GG
BO50P
PACKING: Moisture sensitivity level MSL3
3000 pcs in antistatic tape on a reel packed in a moisture barrier bag (MBB).
Information furnished by Silicon Standard Corporation is believed to be accurate and reliable. However, Silicon Standard Corporation makes no
guarantee or warranty, express or implied, as to the reliability, accuracy, timeliness or completeness of such information and assumes no
responsibility for its use, or for infringement of any patent or other intellectual property rights of third parties that may result from its
use. Silicon Standard reserves the right to make changes as it deems necessary to any products described herein for any reason, including
without limitation enhancement in reliability, functionality or design. No license is granted, whether expressly or by implication, in relation to
the use of any products described herein or to the use of any information provided herein, under any patent or other intellectual property rights of
Silicon Standard Corporation or any third parties.
7/21/2005 Rev.3.01
www.SiliconStandard.com
13 of 13