ATF-33143-BLKG [AVAGO]

Low Noise Pseudomorphic HEMT in a Surface Mount Plastic Package; 低噪声赝HEMT的表面贴装塑料封装
ATF-33143-BLKG
型号: ATF-33143-BLKG
厂家: AVAGO TECHNOLOGIES LIMITED    AVAGO TECHNOLOGIES LIMITED
描述:

Low Noise Pseudomorphic HEMT in a Surface Mount Plastic Package
低噪声赝HEMT的表面贴装塑料封装

晶体 小信号场效应晶体管 射频小信号场效应晶体管 光电二极管 放大器
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ATF-33143  
Low Noise Pseudomorphic HEMT  
in a Surface Mount Plastic Package  
Data Sheet  
Description  
Features  
Avago’s ATF-33143 is a high dynamic range, low noise  
PHEMT housed in a 4-lead SC-70 (SOT-343) surface mount  
plastic package.  
Lead-free Option Available  
Low Noise Figure  
Excellent Uniformity in Product Specifications  
1600 micron Gate Width  
Based on its featured performance, ATF-33143 is ideal for  
the first or second stage of base station LNA due to the  
excellent combination of low noise figure and enhanced  
linearity[1]. The device is also suitable for applications in  
Wireless LAN, WLL/RLL, MMDS, and other systems requiring  
super low noise figure with good intercept in the 450 MHz  
to 10 GHz frequency range.  
Low Cost Surface Mount Small Plastic Package  
SOT-343 (4 lead SC-70)  
Tape-and-Reel Packaging Option Available  
Specifications  
1.9 GHz; 4V, 80 mA (Typ.)  
Note:  
1. From the same PHEMT FET family, the smaller geometry ATF-  
34143 may also be considered for the higher gain performance,  
particularly in the higher frequency band (1.8 GHz and up).  
0.5 dB Noise Figure  
15 dB Associated Gain  
22 dBm Output Power at 1 dB Gain Compression  
33.5 dBm Output 3rd Order Intercept  
Surface Mount Package SOT-343  
Applications  
Tower Mounted Amplifier, Low Noise Amplifier and  
Driver Amplifier for GSM/TDMA/CDMA Base Stations  
LNA for Wireless LAN, WLL/RLL and MMDS  
Applications  
Pin Connections and Package Marking  
General Purpose Discrete PHEMT for other Ultra Low  
DRAIN  
SOURCE  
Noise Applications  
SOURCE  
GATE  
Attention: Observe precautions for  
handling electrostatic sensitive devices.  
ESD Machine Model (Class A)  
ESD Human Body Model (Class 0)  
Refer to Avago Application Note A004R:  
Electrostatic Discharge Damage and Control.  
Note:  
Top View. Package marking provides  
orientation and identification.  
“3P= Device code  
“x” = Datecodecharacter. Anewcharacter  
is assigned for each month, year.  
ATF-33143 Absolute Maximum Ratings[1]  
Notes:  
Absolute  
1. Operation of this device above any one of  
these parameters may cause permanent  
damage.  
Symbol  
VDS  
Parameter  
Units  
V
Maximum  
Drain - Source Voltage[2]  
Gate - Source Voltage[2]  
Gate Drain Voltage[2]  
Drain Current[2]  
5.5  
-5  
2. Assumes DC quiesent conditions.  
VGS  
V
3.  
VGS = 0V  
4. Source lead temperature is 25°C. Derate  
6 mW/°C for TL > 60°C.  
5. Please refer to failure rates in reliability  
section to assess the reliability impact  
VGD  
V
-5  
[3]  
IDS  
mA  
mW  
dBm  
°C  
Idss  
Pdiss  
Pin max  
TCH  
Total Power Dissipation[4]  
600  
20  
of running devices above  
temperature of 140°C.  
a channel  
RF Input Power  
Channel Temperature[5]  
Storage Temperature  
Thermal Resistance[6]  
160  
6. Thermal resistance measured using 150°C  
Liquid Crystal Measurement method.  
TSTG  
jc  
°C  
-65 to 160  
145  
°C/W  
Product Consistency Distribution Charts [8, 9]  
500  
120  
100  
80  
Cpk = 1.7  
Std = 0.05  
+0.6  
V
400  
300  
200  
100  
0
V
+3 Std  
-3 Std  
60  
40  
–0.6  
V
20  
0
0
0
2
4
6
8
0.2  
0.3  
0.4  
0.5  
0.6  
0.7  
0.8  
V
(V)  
DS  
NF (dB)  
[7]  
Figure 1. Typical Pulsed I-V Curves . (VGS = -0.2V per step)  
Figure 2. NF @ 2 GHz, 4 V, 80 mA.  
LSL=0.2, Nominal=0.53, USL=0.8  
100  
120  
Cpk = 1.21  
Std = 0.94  
Cpk = 2.3  
Std = 0.2  
100  
80  
60  
40  
20  
80  
60  
40  
20  
-3 Std  
+3 Std  
-3 Std  
+3 Std  
0
0
31  
33  
35  
29  
37  
13  
14  
15  
GAIN (dB)  
16  
17  
OIP3 (dBm)  
Figure 3. OIP3 @ 2 GHz, 4 V, 80 mA.  
LSL=30.0, Nominal=33.3, USL=37.0  
Figure 4. Gain @ 2 GHz, 4 V, 80 mA.  
LSL=13.5, Nominal=14.8, USL=16.5  
Notes:  
7. Under large signal conditions, VGS may swing positive and the drain current may exceed Idss.These conditions are acceptable as long as the maximum  
Pdiss and Pin max ratings are not exceeded.  
8. Distribution data sample size is 450 samples taken from 9 different wafers. Future wafers allocated to this product may have nominal values  
anywhere within the upper and lower spec limits.  
9. Measurements made on production test board. This circuit represents a trade-off between an optimal noise match and a realizeable match based  
on production test requirements. Circuit losses have been de-embedded from actual measurements.  
10. The probability of a parameter being between 1is 68.3%, between 2ꢀ is 95.4% and between 3ꢀ is 99.7%.  
2
ATF-33143 DC Electrical Specifications TA = 25°C, RF parameters measured in a test circuit for a typical device  
Symbol  
Idss  
Parameters and Test Conditions  
Saturated Drain Current  
Pinchoff Voltage  
Units Min. Typ.[2] Max.  
[1]  
VDS = 1.5 V, VGS = 0 V  
VDS = 1.5 V, IDS = 10% of Idss  
VGS = -0.5 V, VDS = 4 V  
VDS = 1.5 V, gm = Idss /VP  
VGD = 5 V  
mA  
V
175  
237  
305  
-0.35  
[1]  
VP  
-0.65 -0.5  
Id  
Quiescent Bias Current  
Transconductance  
mA  
80  
[1]  
gm  
mmho 360  
μA  
440  
IGDO  
Igss  
Gate to Drain Leakage Current  
Gate Leakage Current  
1000  
600  
0.8  
VGD = VGS = -4 V  
μA  
dB  
42  
f = 2 GHz  
f = 900 MHz  
f = 2 GHz  
V
DS = 4 V, IDS = 80 mA  
DS = 4 V, IDS = 60 mA  
VDS = 4 V, IDS = 80 mA  
DS = 4 V, IDS = 60 mA  
0.5  
0.5  
V
NF  
Ga  
Noise Figure  
dB  
dB  
0.4  
0.4  
V
VDS = 4 V, IDS = 80 mA  
VDS = 4 V, IDS = 60 mA  
13.5  
30  
15  
15  
16.5  
Associated Gain[3]  
f = 900 MHz  
f = 2 GHz  
VDS = 4 V, IDS = 80 mA  
dB  
21  
21  
V
DS = 4 V, IDS = 60 mA  
VDS = 4 V, IDS = 80 mA  
dBm  
dBm  
dBm  
dBm  
33.5  
32  
5 dBm Pout/Tone  
VDS = 4 V, IDS = 60 mA  
Output 3rd Order  
Intercept Point[3]  
OIP3  
P1dB  
f = 900 MHz  
VDS = 4 V, IDS = 80 mA  
VDS = 4 V, IDS = 60 mA  
32.5  
31  
5 dBm Pout/Tone  
f = 2 GHz  
VDS = 4 V, IDS = 80 mA  
VDS = 4 V, IDS = 60 mA  
22  
21  
1 dB Compressed  
Compressed Power[3]  
f = 900 MHz  
VDS = 4 V, IDS = 80 mA  
21  
20  
V
DS = 4 V, IDS = 60 mA  
Notes:  
1. Guaranteed at wafer probe level.  
2. Typical value determined from a sample size of 450 parts from 9 wafers.  
3. Measurements obtained using production test board described in Figure 5.  
50 Ohm  
Input  
50 Ohm  
Input  
Output  
Transmission  
Line Including  
Gate Bias T  
Matching Circuit  
G_mag = 0.20  
G_ang = 124  
(0.3 dB loss)  
Transmission  
Line Including  
Drain Bias T  
(0.5 dB loss)  
DUT  
(0.5 dB loss)  
Figure 5. Block diagram of 2 GHz production test board used for Noise Figure, Associated Gain, P1dB, and OIP3 measurements. This circuit represents a  
trade-off between an optimal noise match and a realizable match based on production test requirements. Circuit losses have been de-embedded from  
actual measurements.  
3
ATF-33143 Typical Performance Curves  
40  
40  
30  
20  
10  
0
2 V  
3 V  
4 V  
30  
20  
10  
2 V  
3 V  
4 V  
0
0
20  
40  
60  
(mA)  
80  
100 120  
0
20  
40  
60  
(mA)  
80  
100 120  
I
I
DSQ  
DSQ  
[1]  
[1]  
Figure 6. OIP3, IIP3 vs. Bias at 2 GHz.  
Figure 7. OIP3, IIP3 vs. Bias at 900 MHz.  
25  
20  
15  
10  
5
25  
20  
15  
10  
5
2 V  
3 V  
4 V  
2 V  
3 V  
4 V  
0
0
0
20  
40  
60  
(mA)  
80  
100 120  
0
20  
40  
60  
(mA)  
80  
100 120  
I
I
DSQ  
DSQ  
[1,2]  
[1,2]  
Figure 8. P1dB vs. Bias at 2 GHz.  
Figure 9. P1dB vs. Bias Tuned for NF @ 4V, 80 mA at  
900 MHz.  
1.4  
1.2  
1.0  
0.8  
0.6  
0.4  
0.2  
0
16  
15  
22  
21  
20  
19  
18  
17  
16  
1.2  
1.0  
0.8  
0.6  
0.4  
0.2  
G
a
14  
13  
12  
11  
10  
G
a
NF  
NF  
2 V  
3 V  
4 V  
2 V  
3 V  
4 V  
0
20  
40  
60  
(mA)  
80  
100 120  
0
20  
40  
60  
(mA)  
80  
100 120  
I
I
DSQ  
DSQ  
[1]  
[1]  
Figure 10. NF and Ga vs. Bias at 2 GHz.  
Figure 11. NF and Ga vs. Bias at 900 MHz.  
Notes:  
1. Measurements made on a fixed tuned production test board that was tuned for optimal gain match with reasonable noise figure at 4V 80 mA  
bias. This circuit represents a trade-off between optimal noise match, maximum gain match and a realizable match based on production test  
board requirements. Circuit losses have been de-embedded from actual measurements.  
2. Quiescent drain current, IDSQ, is set with zero RF drive applied. As P1dB is approached, the drain current may increase or decrease depending on  
frequency and dc bias point. At lower values of IDSQ the device is running closer to class B as power output approaches P1dB. This results in higher  
P1dB and higher PAE (power added efficiency) when compared to a device that is driven by a constant current source as is typically done with  
active biasing.  
4
ATF-33143 Typical Performance Curves, continued  
1.5  
1.0  
0.5  
0
30  
25  
20  
15  
10  
5
80 mA  
60 mA  
80 mA  
60 mA  
0
0
2
4
6
8
10  
0
2
4
6
8
10  
FREQUENCY (GHz)  
FREQUENCY (GHz)  
Figure 12. Fmin vs. Frequency and Current at 4V.  
Figure 13. Associated Gain vs. Frequency and  
Current at 4V.  
40  
25  
2.0  
1.5  
1.0  
0.5  
0
25C  
-40C  
85C  
25C  
-40C  
85C  
35  
30  
25  
20  
15  
20  
15  
10  
5
0
2000  
4000  
6000  
8000  
0
2
4
6
8
10  
FREQUENCY (MHz)  
FREQUENCY (GHz)  
Figure 15. P1dB, OIP3 vs. Frequency and Temp at  
VDS = 4V, IDS = 80 mA.  
Figure 14. Fmin and Ga vs. Frequency and Temp at  
VDS = 4V, IDS = 80 mA.  
3.5  
3.0  
2.5  
2.0  
1.5  
1.0  
0.5  
0
35  
35  
30  
25  
20  
15  
10  
5
P
OIP3  
Gain  
NF  
30  
25  
20  
15  
10  
5
1dB  
3
2
1
0
P
Gain  
NF  
1dB  
OIP3  
0
0
0
20  
40  
60  
(mA)  
80  
100 120  
0
20  
40  
60  
(mA)  
80  
100 120  
I
I
DSQ  
DSQ  
Figure 16. OIP3, P1dB, NF and Gain vs. Bias[1,2] at  
3.9 GHz.  
Figure 17. OIP3, P1dB, NF and Gain vs. Bias[1,2] at  
5.8 GHz.  
Notes:  
1. Measurements made on a fixed tuned test fixture that was tuned for noise figure at 4V 80 mA bias. This circuit represents a trade-off between  
optimal noise match, maximum gain match and a realizable match based on production test requirements. Circuit losses have been de-  
embedded from actual measurements.  
2. Quiescent drain current, IDSQ, is set with zero RF drive applied. As P1dB is approached, the drain current may increase or decrease depending on  
frequency and dc bias point. At lower values of Idsq the device is running closer to class B as power output approaches P1dB. This results in higher  
P1dB and higher PAE (power added efficiency) when compared to a device that is driven by a constant current source as is typically done with  
active biasing.  
5
ATF-33143 Typical Performance Curves, continued  
25  
20  
15  
10  
25  
20  
15  
10  
5
5
0
0
0
20  
40  
60  
80  
100  
120  
0
20  
40  
60  
80  
100  
120  
I
(mA)  
I
(mA)  
DS  
DS  
Figure 19. P1dB vs. IDS Active Bias[1] Tuned for NF @  
4V, 80 mA at 900 MHz.  
Figure 18. P1dB vs. IDS Active Bias[1] Tuned for NF @  
4V, 80 mA at 2 GHz.  
Note:  
1. Measurements made on a fixed tuned test board that was tuned for optimal gain match with reasonable noise figure at 4V 80 mA bias. This  
circuit represents a trade-off between an optimal noise match, maximum gain match and a realizable match based on production test board  
requirements. Circuit losses have been de-embedded from actual measurements.  
6
ATF-33143 Power Parameters Tuned for Max P1dB, VDS = 4 V, IDSQ = 80 mA  
Freq  
(GHz)  
P1dB  
(dBm)  
Id  
(mA)  
G1dB  
(dB)  
PAE1dB  
(%)  
P3dB  
(dBm)  
Id  
(mA)  
PAE3dB  
(%)  
Out_mag  
(Mag.)  
Out_ang  
(°)  
0.9  
1.5  
1.8  
2.0  
4.0  
6.0  
20.7  
21.2  
21.1  
21.6  
23.0  
24.0  
89  
91  
80  
81  
97  
23.2  
20.7  
19.2  
18.1  
11.9  
5.9  
33  
36  
40  
44  
48  
36  
23.2  
23.8  
23.0  
23.2  
24.6  
25.2  
102  
116  
94  
89  
135  
136  
51  
51  
52  
57  
48  
36  
0.39  
0.43  
0.43  
0.42  
0.40  
0.37  
160  
165  
170  
174  
-150  
-124  
130  
70  
P
Gain  
PAE  
out  
60  
50  
40  
30  
20  
10  
0
-10  
-20  
-40  
-30  
-20  
-10  
0
10  
20  
P
in  
(dBm)  
Figure 20. Swept Power Tuned for Max P  
1dB  
V
=4V, I = 80 mA, 2 GHz.  
DS  
DSQ  
Notes:  
1. Measurements made on ATN LP1 power load pull system.  
2. Quicescent drain current, IDSQ, is set with zero RF drive applied. As P1dB is approached, the drain current may increase or decrease depending  
on frequency and dc bias point. At lower values of IDSQ the device is running closer to class B as power output approaches P1dB. This results in  
higher P1dB and higher PAE (power added efficiency) when compared to a device that is driven by a constant current source as is typically done  
with active biasing.  
3. PAE (%) = ((Pout – Pin) / Pdc) X 100  
4. Gamma out is the reflection coefficient of the matching circuit presented to the output of the device.  
7
ATF-33143 Typical Scattering Parameters, VDS = 2V, IDS = 40 mA  
Freq.  
(GHz)  
S11  
S21  
Mag.  
S12  
Mag.  
S22  
MSG/MAG  
(dB)  
Mag.  
Ang.  
dB  
Ang.  
dB  
Ang.  
Mag.  
Ang.  
0.5  
0.8  
1.0  
1.5  
1.8  
2.0  
2.5  
3.0  
4.0  
5.0  
6.0  
7.0  
8.0  
0.88  
0.79  
0.78  
0.75  
0.74  
0.74  
0.74  
0.75  
0.75  
0.76  
0.78  
0.80  
0.83  
0.83  
0.86  
0.88  
0.90  
0.91  
0.91  
0.92  
0.93  
0.94  
0.93  
-72.70  
22.08 12.81  
134.40  
111.20  
106.50  
88.30  
79.80  
74.80  
63.00  
53.10  
35.00  
17.20  
-1.30  
-19.30  
-35.20  
-49.30  
-64.30  
-80.20  
-95.80  
-27.02  
-24.13  
-23.93  
-22.57  
-22.14  
-21.84  
-21.24  
-20.68  
-19.59  
-18.56  
-17.83  
-17.42  
-17.29  
-17.08  
-16.59  
-16.53  
-16.81  
-17.38  
-17.78  
-18.00  
-17.87  
-18.07  
-18.79  
0.045  
0.062  
0.064  
0.075  
0.079  
0.082  
0.088  
0.094  
0.106  
0.119  
0.129  
0.135  
0.137  
0.140  
0.148  
0.149  
0.144  
0.135  
54.50  
40.70  
38.00  
29.80  
26.80  
24.90  
20.80  
17.10  
9.30  
0.28  
0.37  
0.38  
0.42  
0.45  
0.46  
0.49  
0.51  
0.53  
0.54  
0.54  
0.57  
0.60  
0.63  
0.65  
0.68  
0.72  
0.75  
0.77  
0.80  
0.82  
0.83  
0.85  
-118.70  
-149.90  
-155.40  
-176.20  
174.70  
169.40  
160.10  
152.10  
139.20  
124.70  
108.00  
90.40  
74.80  
62.70  
50.90  
37.40  
21.40  
5.80  
-5.70  
24.54  
21.81  
21.41  
19.34  
18.40  
17.80  
16.56  
15.46  
13.73  
11.44  
9.80  
8.35  
7.43  
6.45  
6.41  
6.14  
5.64  
4.60  
3.64  
-112.10  
-119.80  
-149.60  
-162.80  
-170.10  
172.30  
159.10  
137.00  
117.20  
98.10  
80.10  
64.50  
50.30  
36.30  
21.50  
7.20  
-5.00  
19.46  
18.86  
16.11  
14.70  
13.84  
11.98  
10.37  
7.95  
6.20  
4.69  
3.12  
1.68  
9.41  
8.86  
6.44  
5.47  
4.94  
3.98  
3.31  
2.50  
2.05  
1.73  
1.44  
1.22  
1.07  
0.96  
0.85  
0.74  
-0.70  
-12.80  
-26.00  
-37.30  
-46.80  
-58.30  
-71.30  
-83.90  
-95.60  
9.0  
0.48  
10.0  
11.0  
12.0  
13.0  
14.0  
15.0  
16.0  
17.0  
18.0  
-0.46  
-1.50  
-2.70  
-4.24  
-5.49  
-6.42  
-7.26  
-8.20  
-9.51  
0.62 -110.20  
0.54 -121.90  
0.49 -134.20  
0.44 -146.80  
0.40 -160.40  
0.34 -171.00  
-15.50  
-27.50  
-40.50  
-52.30  
-61.20  
0.129 -103.90  
0.126 -113.70  
0.128 -124.20  
0.125 -136.40  
0.115 -145.10  
-15.80  
-25.70  
-37.90  
-49.70  
3.44  
3.22  
3.11  
1.79  
ATF-33143 Typical Noise Parameters  
VDS = 2V, IDS = 40 mA  
40  
30  
20  
10  
0
Freq.  
GHz  
Fmin      opt  
dB  
Rn/50  
-
Ga  
dB  
Mag.  
Ang.  
26.00  
42.20  
44.80  
69.50  
MSG  
0.5  
0.9  
1.0  
1.5  
1.8  
2.0  
2.5  
3.0  
4.0  
5.0  
6.0  
7.0  
8.0  
9.0  
10.0  
0.26  
0.30  
0.31  
0.34  
0.34  
0.39  
0.51  
0.53  
0.61  
0.70  
0.82  
0.93  
1.04  
1.12  
1.21  
0.45  
0.38  
0.36  
0.31  
0.26  
0.27  
0.28  
0.32  
0.41  
0.49  
0.53  
0.59  
0.62  
0.67  
0.69  
0.07  
0.07  
0.07  
0.06  
0.04  
0.05  
0.03  
0.03  
0.04  
0.06  
0.11  
0.23  
0.38  
0.59  
0.77  
24.74  
21.02  
20.36  
17.40  
16.50  
15.82  
14.59  
13.13  
11.27  
9.92  
MAG  
93.60  
108.60  
150.70  
165.60  
-162.10  
-136.80  
-113.60  
-91.50  
-72.60  
-55.90  
-42.20  
2
|S  
|
21  
-10  
0
5
10  
FREQUENCY (GHz)  
15  
20  
Figure 21. MSG/MAG and |S21|  
2 vs. Frequency at 2V, 40 mA.  
8.70  
7.71  
6.69  
6.04  
5.73  
Notes:  
1. The Fmin values are based on a set of 16 noise figure measurements made at 16 different impedances using an ATF NP5 test system. From these  
measurements a true Fmin is calculated. Refer to the noise parameter application section for more information.  
2. S and noise parameters are measured on a microstrip line made on 0.025 inch thick alumina carrier. The input reference plane is at the end  
of the gate lead. The output reference plane is at the end of the drain lead. The parameters include the effect of four plated through via holes  
connecting source landing pads on top of the test carrier to the microstrip ground plane on the bottom side of the carrier. Two 0.020 inch  
diameter via holes are placed within 0.010 inch from each source lead contact point, one via on each side of that point.  
8
ATF-33143 Typical Scattering Parameters, VDS = 3 V, IDS = 40 mA  
Freq.  
(GHz)  
S11  
S21  
Mag.  
S12  
Mag.  
S22  
MSG/MAG  
(dB)  
Mag.  
Ang.  
dB  
Ang.  
dB  
Ang.  
Mag.  
Ang.  
0.5  
0.8  
1.0  
1.5  
1.8  
2.0  
2.5  
3.0  
4.0  
5.0  
6.0  
7.0  
8.0  
0.87  
0.78  
0.77  
0.74  
0.73  
0.73  
0.73  
0.74  
0.74  
0.75  
0.77  
0.79  
0.82  
0.83  
0.86  
0.88  
0.90  
0.91  
0.91  
0.92  
0.93  
0.94  
0.93  
-72.20  
22.51 13.42  
134.40  
111.20  
106.50  
88.30  
79.90  
74.80  
63.10  
53.30  
35.20  
17.30  
-1.30  
-19.50  
-35.50  
-49.60  
-64.90  
-81.00  
-96.80  
-27.20  
-24.27  
-24.06  
-22.79  
-22.34  
-22.13  
-21.41  
-20.91  
-19.79  
-18.80  
-17.99  
-17.58  
-17.44  
-17.13  
-16.64  
-16.58  
-16.81  
-17.38  
-17.78  
-17.93  
-17.87  
-18.00  
-18.72  
0.044  
0.061  
0.063  
0.073  
0.077  
0.079  
0.086  
0.091  
0.103  
0.115  
0.126  
0.132  
0.134  
0.139  
0.147  
0.148  
0.144  
0.135  
54.40  
40.60  
37.90  
29.80  
26.90  
25.00  
21.10  
17.50  
10.00  
0.00  
-11.90  
-24.90  
-36.00  
-45.50  
-57.00  
-70.10  
-82.70  
-94.40  
0.27  
0.35  
0.36  
0.40  
0.42  
0.43  
0.46  
0.48  
0.50  
0.51  
0.52  
0.55  
0.57  
0.60  
0.63  
0.66  
0.70  
0.73  
0.76  
0.79  
0.81  
0.82  
0.84  
-109.80  
-143.70  
-150.10  
-172.10  
178.40  
172.90  
163.10  
154.80  
141.20  
126.50  
109.80  
92.10  
76.20  
64.00  
52.10  
38.60  
22.60  
6.80  
-5.00  
24.84  
22.09  
21.67  
19.64  
18.71  
18.16  
16.85  
15.80  
14.06  
11.53  
9.99  
8.57  
7.64  
6.69  
6.65  
6.38  
6.00  
4.90  
3.90  
-111.60  
-119.30  
-149.00  
-162.20  
-169.50  
172.90  
159.70  
137.60  
117.70  
98.60  
80.60  
64.90  
50.70  
36.60  
21.90  
7.50  
-4.80  
19.88  
19.28  
16.52  
15.11  
14.24  
12.38  
10.78  
8.37  
6.63  
5.10  
3.54  
2.10  
9.87  
9.26  
6.73  
5.72  
5.17  
4.17  
3.46  
2.62  
2.15  
1.80  
1.51  
1.28  
1.12  
1.00  
0.89  
0.77  
9.0  
0.92  
10.0  
11.0  
12.0  
13.0  
14.0  
15.0  
16.0  
17.0  
18.0  
-0.04  
-1.11  
-2.32  
-3.86  
-5.11  
-6.05  
-6.95  
-7.91  
-9.25  
0.64 -111.40  
0.56 -123.30  
0.50 -135.90  
0.45 -148.70  
0.41 -162.30  
0.35 -172.90  
-15.40  
-27.40  
-40.40  
-52.30  
-61.30  
0.129 -103.00  
0.127 -112.80  
0.128 -123.40  
0.126 -135.70  
0.116 -144.30  
-15.10  
-25.10  
-37.30  
-49.10  
3.71  
3.48  
3.41  
1.94  
ATF-33143 Typical Noise Parameters  
VDS = 3V, IDS = 40 mA  
40  
30  
Freq.  
GHz  
Fmin      opt  
Rn/50  
-
Ga  
dB  
dB  
Mag.  
Ang.  
MSG  
0.5  
0.9  
1.0  
1.5  
1.8  
2.0  
2.5  
3.0  
4.0  
5.0  
6.0  
7.0  
8.0  
9.0  
10.0  
0.24  
0.29  
0.31  
0.37  
0.34  
0.38  
0.51  
0.52  
0.58  
0.68  
0.80  
0.89  
1.01  
1.09  
1.18  
0.45  
0.38  
0.34  
0.28  
0.25  
0.25  
0.28  
0.31  
0.40  
0.46  
0.54  
0.57  
0.61  
0.65  
0.68  
28.40  
40.90  
42.60  
66.30  
90.10  
105.80  
147.40  
162.80  
-165.20  
-138.50  
-115.00  
-92.50  
-72.80  
-56.40  
-42.60  
0.07  
0.07  
0.07  
0.07  
0.05  
0.05  
0.03  
0.03  
0.03  
0.05  
0.09  
0.20  
0.35  
0.53  
0.69  
25.26  
21.26  
20.50  
17.67  
16.57  
15.93  
14.72  
13.29  
11.45  
10.05  
8.97  
20  
10  
0
MAG  
2
|S  
|
21  
-10  
5
10  
FREQUENCY (GHz)  
15  
0
20  
Figure 22. MSG/MAG and |S21|  
2 vs. Frequency at 3V, 40 mA.  
7.90  
6.90  
6.26  
5.99  
Notes:  
1. The Fmin values are based on a set of 16 noise figure measurements made at 16 different impedances using an ATF NP5 test system. From these  
measurements a true Fmin is calculated. Refer to the noise parameter application section for more information.  
2. S and noise parameters are measured on a microstrip line made on 0.025 inch thick alumina carrier. The input reference plane is at the end  
of the gate lead. The output reference plane is at the end of the drain lead. The parameters include the effect of four plated through via holes  
connecting source landing pads on top of the test carrier to the microstrip ground plane on the bottom side of the carrier. Two 0.020 inch  
diameter via holes are placed within 0.010 inch from each source lead contact point, one via on each side of that point.  
9
ATF-33143 Typical Scattering Parameters, VDS = 3 V, IDS = 60 mA  
Freq.  
(GHz)  
S11  
S21  
Mag.  
S12  
Mag.  
S22  
MSG/MAG  
(dB)  
Mag.  
Ang.  
dB  
Ang.  
dB  
Ang.  
Mag.  
Ang.  
0.5  
0.8  
1.0  
1.5  
1.8  
2.0  
2.5  
3.0  
4.0  
5.0  
6.0  
7.0  
8.0  
0.87  
0.78  
0.77  
0.74  
0.73  
0.73  
0.73  
0.74  
0.75  
0.75  
0.77  
0.79  
0.82  
0.83  
0.86  
0.88  
0.90  
0.91  
0.91  
0.92  
0.93  
0.94  
0.93  
-75.30  
22.95 14.06  
20.22 10.26  
133.00  
110.00  
105.50  
87.60  
79.30  
74.40  
62.80  
53.10  
35.40  
17.70  
-0.60  
-18.60  
-34.40  
-48.50  
-63.50  
-79.50  
-95.10  
-28.18  
-25.19  
-24.89  
-23.37  
-22.87  
-22.53  
-21.76  
-21.07  
-19.79  
-18.68  
-17.88  
-17.42  
-17.29  
-17.03  
-16.49  
-16.43  
-16.71  
-17.27  
-17.72  
-17.86  
-17.72  
-17.92  
-18.64  
0.039  
0.055  
0.057  
0.068  
0.072  
0.075  
0.082  
0.089  
0.103  
0.117  
0.128  
0.135  
0.137  
0.141  
0.150  
0.151  
0.146  
0.137  
55.10  
42.60  
40.50  
33.50  
30.80  
29.00  
25.10  
21.40  
13.20  
2.80  
0.27  
0.36  
0.37  
0.41  
0.43  
0.44  
0.47  
0.50  
0.52  
0.52  
0.53  
0.56  
0.59  
0.62  
0.65  
0.68  
0.71  
0.74  
0.77  
0.80  
0.82  
0.82  
0.84  
-124.20  
-153.90  
-158.80  
-178.70  
172.60  
167.50  
158.50  
151.00  
138.60  
124.40  
107.80  
90.20  
74.70  
62.70  
50.90  
37.40  
21.40  
5.80  
-6.10  
25.57  
22.71  
22.24  
20.07  
19.11  
18.49  
17.17  
16.00  
14.15  
11.53  
10.03  
8.66  
7.75  
6.81  
6.72  
6.46  
6.04  
4.99  
3.98  
3.78  
-114.70  
-122.30  
-151.60  
-164.60  
-171.80  
171.00  
158.10  
136.40  
116.90  
97.80  
79.90  
64.50  
50.40  
36.40  
21.60  
7.30  
-5.00  
19.59  
16.78  
15.35  
14.47  
12.60  
10.99  
8.56  
6.80  
5.28  
3.71  
2.26  
9.56  
6.91  
5.87  
5.30  
4.27  
3.54  
2.68  
2.19  
1.84  
1.53  
1.30  
1.13  
1.02  
0.90  
0.78  
-9.70  
-23.20  
-34.60  
-44.50  
-56.20  
-69.40  
-82.10  
-94.00  
9.0  
1.07  
0.12  
10.0  
11.0  
12.0  
13.0  
14.0  
15.0  
16.0  
17.0  
18.0  
-0.94  
-2.13  
-3.67  
-4.93  
-5.85  
-6.70  
-7.61  
-8.97  
0.66 -109.70  
0.57 -121.40  
0.51 -133.90  
0.46 -146.60  
0.42 -160.30  
0.36 -170.90  
-15.50  
-27.50  
-40.60  
-52.30  
-61.40  
0.130 -102.70  
0.128 -112.40  
0.130 -123.00  
0.127 -135.30  
0.117 -144.00  
-15.80  
-25.80  
-37.90  
-49.70  
3.54  
3.45  
2.08  
ATF-33143 Typical Noise Parameters  
VDS = 3V, IDS = 60 mA  
40  
30  
Freq.  
GHz  
Fmin      opt  
Rn/50  
-
Ga  
dB  
dB  
Mag.  
Ang.  
MSG  
20  
10  
0
0.5  
0.9  
1.0  
1.5  
1.8  
2.0  
2.5  
3.0  
4.0  
5.0  
6.0  
7.0  
8.0  
9.0  
10.0  
0.23  
0.28  
0.29  
0.34  
0.34  
0.38  
0.52  
0.53  
0.61  
0.68  
0.83  
0.91  
1.04  
1.09  
1.13  
0.43  
0.35  
0.35  
0.26  
0.23  
0.22  
0.25  
0.30  
0.39  
0.47  
0.52  
0.58  
0.61  
0.66  
0.70  
29.20  
42.40  
45.00  
68.80  
93.30  
109.70  
150.60  
167.50  
-160.30  
-134.70  
-112.10  
-89.70  
-71.50  
-54.80  
-41.40  
0.06  
0.06  
0.07  
0.06  
0.04  
0.05  
0.03  
0.03  
0.04  
0.06  
0.11  
0.22  
0.36  
0.56  
0.73  
25.64  
21.62  
20.87  
17.84  
16.89  
16.24  
14.93  
13.52  
11.65  
10.28  
9.09  
MAG  
2
|S  
|
21  
-10  
5
10  
FREQUENCY (GHz)  
15  
0
20  
Figure 23. MSG/MAG and |S21|  
2 vs. Frequency at 3V, 60 mA.  
8.09  
7.07  
6.43  
6.15  
Notes:  
1. The Fmin values are based on a set of 16 noise figure measurements made at 16 different impedances using an ATF NP5 test system. From these  
measurements a true Fmin is calculated. Refer to the noise parameter application section for more information.  
2. S and noise parameters are measured on a microstrip line made on 0.025 inch thick alumina carrier. The input reference plane is at the end  
of the gate lead. The output reference plane is at the end of the drain lead. The parameters include the effect of four plated through via holes  
connecting source landing pads on top of the test carrier to the microstrip ground plane on the bottom side of the carrier. Two 0.020 inch  
diameter via holes are placed within 0.010 inch from each source lead contact point, one via on each side of that point.  
10  
ATF-33143 Typical Scattering Parameters, VDS = 4 V, IDS = 40 mA  
Freq.  
(GHz)  
S11  
S21  
Mag.  
S12  
Mag.  
S22  
MSG/MAG  
(dB)  
Mag.  
Ang.  
dB  
Ang.  
dB  
Ang.  
Mag.  
Ang.  
0.5  
0.8  
1.0  
1.5  
1.8  
2.0  
2.5  
3.0  
4.0  
5.0  
6.0  
7.0  
8.0  
0.87  
0.78  
0.77  
0.73  
0.72  
0.72  
0.72  
0.73  
0.74  
0.75  
0.77  
0.79  
0.82  
0.83  
0.86  
0.88  
0.90  
0.91  
0.91  
0.92  
0.93  
0.94  
0.93  
-72.50  
22.73 13.74  
20.07 10.09  
134.30  
111.00  
106.40  
88.20  
79.80  
74.70  
63.00  
53.20  
35.10  
17.10  
-1.60  
-19.80  
-35.90  
-50.20  
-65.60  
-81.80  
-97.60  
-27.39  
-24.42  
-24.20  
-22.90  
-22.44  
-22.23  
-21.58  
-21.07  
-19.93  
-18.92  
-18.11  
-17.68  
-17.50  
-17.23  
-16.69  
-16.58  
-16.81  
-17.32  
-17.78  
-17.93  
-17.79  
-18.00  
-18.72  
0.043  
0.060  
0.062  
0.072  
0.076  
0.078  
0.084  
0.089  
0.101  
0.113  
0.124  
0.130  
0.133  
0.137  
0.146  
0.148  
0.144  
0.136  
54.10  
40.40  
37.70  
29.80  
26.90  
25.00  
21.20  
17.80  
10.40  
0.70  
-11.20  
-24.10  
-35.10  
-44.60  
-56.10  
-69.10  
-81.70  
-93.50  
0.26  
0.33  
0.34  
0.38  
0.40  
0.41  
0.44  
0.46  
0.48  
0.49  
0.50  
0.53  
0.56  
0.59  
0.62  
0.65  
0.69  
0.72  
0.76  
0.79  
0.81  
0.82  
0.84  
-104.90  
-140.20  
-147.10  
-169.70  
-179.30  
175.10  
165.10  
156.50  
142.50  
127.70  
111.00  
93.40  
77.30  
64.90  
53.00  
39.50  
23.50  
7.50  
-4.30  
25.04  
22.26  
21.82  
19.78  
18.84  
18.29  
17.03  
15.98  
14.23  
11.54  
10.07  
8.68  
7.77  
6.80  
6.78  
6.55  
6.13  
5.03  
4.06  
3.87  
-111.80  
-119.40  
-149.10  
-162.20  
-169.50  
173.00  
159.80  
137.70  
117.90  
98.80  
80.80  
65.10  
50.90  
36.80  
22.00  
7.60  
-4.70  
19.46  
16.69  
15.28  
14.41  
12.55  
10.95  
8.54  
6.80  
5.28  
3.72  
2.29  
9.43  
6.85  
5.82  
5.26  
4.24  
3.53  
2.68  
2.19  
1.84  
1.54  
1.30  
1.14  
1.02  
0.90  
0.78  
9.0  
1.10  
0.15  
10.0  
11.0  
12.0  
13.0  
14.0  
15.0  
16.0  
17.0  
18.0  
-0.93  
-2.14  
-3.69  
-4.97  
-5.92  
-6.85  
-7.83  
-9.19  
0.66 -112.40  
0.57 -124.50  
0.51 -137.30  
0.46 -150.10  
0.41 -163.80  
0.35 -174.60  
-15.30  
-27.20  
-40.30  
-52.20  
-61.20  
0.129 -102.10  
0.127 -112.20  
0.129 -122.80  
0.126 -135.10  
0.116 -143.80  
-14.60  
-24.50  
-36.80  
-48.70  
3.62  
3.54  
2.05  
ATF-33143 Typical Noise Parameters  
VDS = 4V, IDS = 40 mA  
40  
30  
Freq.  
GHz  
Fmin      opt  
Rn/50  
-
Ga  
dB  
MSG  
dB  
Mag.  
Ang.  
20  
10  
0
0.5  
0.9  
1.0  
1.5  
1.8  
2.0  
2.5  
3.0  
4.0  
5.0  
6.0  
7.0  
8.0  
9.0  
10.0  
0.30  
0.33  
0.34  
0.38  
0.37  
0.40  
0.53  
0.54  
0.60  
0.68  
0.82  
0.89  
1.00  
1.07  
1.16  
0.44  
0.36  
0.33  
0.26  
0.25  
0.23  
0.27  
0.31  
0.38  
0.46  
0.49  
0.56  
0.60  
0.66  
0.68  
31.50  
42.70  
44.50  
68.70  
90.70  
106.40  
145.80  
162.00  
-165.30  
-138.80  
-115.40  
-93.20  
-73.10  
-56.60  
-42.80  
0.08  
0.07  
0.08  
0.06  
0.05  
0.05  
0.04  
0.03  
0.04  
0.05  
0.09  
0.19  
0.33  
0.50  
0.65  
25.59  
21.43  
20.63  
17.72  
16.65  
15.99  
14.70  
13.32  
11.47  
10.17  
8.93  
MAG  
2
|S  
|
21  
-10  
5
10  
FREQUENCY (GHz)  
15  
0
20  
Figure 24. MSG/MAG and |S21|  
2 vs. Frequency at 4V, 40 mA.  
7.99  
7.00  
6.40  
6.11  
Notes:  
1. The Fmin values are based on a set of 16 noise figure measurements made at 16 different impedances using an ATF NP5 test system. From these  
measurements a true Fmin is calculated. Refer to the noise parameter application section for more information.  
2. S and noise parameters are measured on a microstrip line made on 0.025 inch thick alumina carrier. The input reference plane is at the end  
of the gate lead. The output reference plane is at the end of the drain lead. The parameters include the effect of four plated through via holes  
connecting source landing pads on top of the test carrier to the microstrip ground plane on the bottom side of the carrier. Two 0.020 inch  
diameter via holes are placed within 0.010 inch from each source lead contact point, one via on each side of that point.  
11  
ATF-33143 Typical Scattering Parameters, VDS = 4 V, IDS = 60 mA  
Freq.  
(GHz)  
S11  
S21  
Mag.  
S12  
Mag.  
S22  
MSG/MAG  
(dB)  
Mag.  
Ang.  
dB  
Ang.  
dB  
Ang.  
Mag.  
Ang.  
0.5  
0.8  
1.0  
1.5  
1.8  
2.0  
2.5  
3.0  
4.0  
5.0  
6.0  
7.0  
8.0  
0.86  
0.77  
0.76  
0.73  
0.72  
0.72  
0.72  
0.73  
0.74  
0.75  
0.77  
0.79  
0.82  
0.83  
0.86  
0.88  
0.90  
0.91  
0.91  
0.92  
0.93  
0.94  
0.93  
-75.60  
23.20 14.45  
20.45 10.53  
132.90  
109.80  
105.30  
87.50  
79.20  
74.20  
62.70  
53.00  
35.20  
17.50  
-1.00  
-19.00  
-34.90  
-49.10  
-64.30  
-80.40  
-96.20  
-28.18  
-25.35  
-25.04  
-23.61  
-22.97  
-22.73  
-21.94  
-21.31  
-20.00  
-18.86  
-17.99  
-17.52  
-17.39  
-17.08  
-16.54  
-16.48  
-16.71  
-17.27  
-17.65  
-17.79  
-17.72  
-17.92  
-18.56  
0.039  
0.054  
0.056  
0.066  
0.071  
0.073  
0.080  
0.086  
0.100  
0.114  
0.126  
0.133  
0.135  
0.140  
0.149  
0.150  
0.146  
0.137  
54.80  
42.20  
40.20  
33.20  
30.60  
28.90  
25.10  
21.60  
13.70  
3.40  
0.26  
0.34  
0.35  
0.39  
0.41  
0.42  
0.45  
0.47  
0.49  
0.50  
0.51  
0.54  
0.57  
0.60  
0.63  
0.66  
0.70  
0.73  
0.76  
0.79  
0.81  
0.82  
0.84  
-118.50  
-150.00  
-155.50  
-176.10  
175.00  
169.80  
160.60  
152.70  
139.90  
125.70  
109.10  
91.60  
75.90  
63.70  
52.00  
38.50  
22.50  
6.70  
-5.20  
25.69  
22.90  
22.42  
20.29  
19.26  
18.70  
17.36  
16.24  
13.79  
11.57  
10.15  
8.80  
7.88  
6.92  
6.92  
6.69  
6.27  
5.14  
4.12  
3.90  
-115.00  
-122.50  
-151.80  
-164.60  
-171.80  
171.00  
158.20  
136.50  
117.00  
98.00  
80.20  
64.70  
50.60  
36.60  
21.80  
7.50  
-4.80  
19.80  
16.98  
15.55  
14.66  
12.79  
11.17  
8.76  
7.00  
5.48  
3.92  
2.48  
9.77  
7.06  
5.99  
5.41  
4.36  
3.62  
2.74  
2.24  
1.88  
1.57  
1.33  
1.16  
1.04  
0.92  
0.80  
-8.90  
-22.30  
-33.60  
-43.40  
-55.20  
-68.40  
-81.10  
-92.90  
9.0  
1.29  
0.34  
10.0  
11.0  
12.0  
13.0  
14.0  
15.0  
16.0  
17.0  
18.0  
-0.72  
-1.94  
-3.48  
-4.73  
-5.68  
-6.56  
-7.54  
-8.87  
0.67 -110.80  
0.58 -122.80  
0.52 -135.40  
0.47 -148.30  
0.42 -162.10  
0.36 -172.80  
-15.40  
-27.30  
-40.40  
-52.20  
-61.20  
0.131 -101.60  
0.129 -111.60  
0.130 -122.20  
0.127 -134.70  
0.118 -143.30  
-15.20  
-25.10  
-37.30  
-49.20  
3.72  
3.59  
2.19  
ATF-33143 Typical Noise Parameters  
VDS = 4V, IDS = 60 mA  
40  
30  
Freq.  
GHz  
Fmin      opt  
Rn/50  
-
Ga  
dB  
dB  
Mag.  
Ang.  
MSG  
0.5  
0.9  
1.0  
1.5  
1.8  
2.0  
2.5  
3.0  
4.0  
5.0  
6.0  
7.0  
8.0  
9.0  
10.0  
0.29  
0.33  
0.34  
0.38  
0.39  
0.42  
0.47  
0.51  
0.63  
0.72  
0.82  
0.93  
1.03  
1.13  
1.22  
0.42  
0.33  
0.32  
0.26  
0.22  
0.22  
0.25  
0.29  
0.39  
0.46  
0.51  
0.57  
0.61  
0.66  
0.69  
31.40  
44.70  
48.00  
71.90  
94.00  
109.70  
149.40  
166.80  
-160.60  
-135.30  
-112.40  
-90.90  
-71.80  
-55.50  
-41.80  
0.08  
0.07  
0.07  
0.06  
0.05  
0.05  
0.03  
0.03  
0.04  
0.06  
0.11  
0.21  
0.37  
0.55  
0.72  
25.91  
21.80  
21.00  
18.14  
16.96  
16.29  
14.95  
13.58  
11.74  
10.36  
9.17  
20  
10  
0
MAG  
2
|S  
|
21  
-10  
5
10  
FREQUENCY (GHz)  
15  
0
20  
Figure 25. MSG/MAG and |S21|  
2 vs. Frequency at 4V, 60 mA.  
8.18  
7.19  
6.56  
6.29  
Notes:  
1. The Fmin values are based on a set of 16 noise figure measurements made at 16 different impedances using an ATF NP5 test system. From these  
measurements a true Fmin is calculated. Refer to the noise parameter application section for more information.  
2. S and noise parameters are measured on a microstrip line made on 0.025 inch thick alumina carrier. The input reference plane is at the end  
of the gate lead. The output reference plane is at the end of the drain lead. The parameters include the effect of four plated through via holes  
connecting source landing pads on top of the test carrier to the microstrip ground plane on the bottom side of the carrier. Two 0.020 inch  
diameter via holes are placed within 0.010 inch from each source lead contact point, one via on each side of that point.  
12  
ATF-33143 Typical Scattering Parameters, VDS = 4 V, IDS = 80 mA  
Freq.  
(GHz)  
S11  
S21  
Mag.  
S12  
Mag.  
S22  
MSG/MAG  
(dB)  
Mag.  
Ang.  
dB  
Ang.  
dB  
Ang.  
Mag.  
Ang.  
0.5  
0.8  
1.0  
1.5  
1.8  
2.0  
2.5  
3.0  
4.0  
5.0  
6.0  
7.0  
8.0  
0.86  
0.77  
0.76  
0.73  
0.72  
0.72  
0.72  
0.73  
0.74  
0.75  
0.77  
0.79  
0.82  
0.83  
0.86  
0.88  
0.90  
0.91  
0.91  
0.92  
0.93  
0.94  
0.93  
-77.20  
23.39 14.76  
20.60 10.71  
132.20  
109.20  
104.80  
87.10  
78.90  
74.00  
62.50  
53.00  
35.30  
17.70  
-0.70  
-18.70  
-34.50  
-48.70  
-63.80  
-79.90  
-95.60  
-28.82  
-25.86  
-25.49  
-23.86  
-23.31  
-22.95  
-22.03  
-21.39  
-20.00  
-18.86  
-17.99  
-17.47  
-17.34  
-17.03  
-16.49  
-16.38  
-16.66  
-17.21  
-17.59  
-17.79  
-17.65  
-17.85  
-18.56  
0.036  
0.051  
0.053  
0.064  
0.068  
0.071  
0.079  
0.085  
0.100  
0.114  
0.126  
0.134  
0.136  
0.141  
0.150  
0.152  
0.147  
0.138  
55.30  
43.40  
41.70  
35.20  
32.70  
31.00  
27.20  
23.50  
15.30  
4.80  
0.26  
0.34  
0.36  
0.39  
0.41  
0.42  
0.45  
0.48  
0.50  
0.51  
0.52  
0.55  
0.58  
0.61  
0.63  
0.66  
0.70  
0.73  
0.76  
0.79  
0.81  
0.82  
0.84  
-125.40  
-154.80  
-159.50  
-179.10  
172.40  
167.30  
158.50  
151.00  
138.80  
124.80  
108.40  
90.90  
75.40  
63.30  
51.60  
38.10  
22.10  
6.40  
-5.00  
26.13  
23.22  
22.72  
20.48  
19.50  
18.87  
17.47  
16.34  
13.59  
11.56  
10.17  
8.84  
7.93  
6.98  
6.96  
6.73  
6.26  
5.21  
4.20  
3.98  
-116.60  
-124.00  
-153.00  
-165.80  
-172.90  
170.10  
157.40  
136.00  
116.70  
97.70  
80.00  
64.50  
50.50  
36.50  
21.70  
7.40  
-4.80  
19.93  
17.09  
15.66  
14.77  
12.89  
11.27  
8.84  
7.09  
5.57  
4.00  
2.55  
9.91  
7.15  
6.06  
5.47  
4.41  
3.66  
2.77  
2.26  
1.90  
1.58  
1.34  
1.17  
1.05  
0.93  
0.81  
-7.80  
-21.30  
-32.80  
-42.80  
-54.60  
-67.80  
-80.60  
-92.60  
9.0  
1.36  
0.43  
10.0  
11.0  
12.0  
13.0  
14.0  
15.0  
16.0  
17.0  
18.0  
-0.65  
-1.85  
-3.39  
-4.64  
-5.57  
-6.46  
-7.40  
-8.75  
0.68 -110.20  
0.59 -122.00  
0.53 -134.80  
0.47 -147.60  
0.43 -161.40  
0.36 -172.10  
-15.40  
-27.30  
-40.40  
-52.20  
-61.20  
0.132 -101.10  
0.129 -111.20  
0.131 -121.90  
0.128 -134.30  
0.118 -143.10  
-15.40  
-25.30  
-37.50  
-49.30  
3.73  
3.65  
2.24  
ATF-33143 Typical Noise Parameters  
VDS = 4V, IDS = 80 mA  
40  
30  
20  
10  
0
Freq.  
GHz  
Fmin      opt  
Rn/50  
-
Ga  
dB  
dB  
Mag.  
Ang.  
34.50  
46.40  
50.40  
74.80  
MSG  
0.5  
0.9  
1.0  
1.5  
1.8  
2.0  
2.5  
3.0  
4.0  
5.0  
6.0  
7.0  
8.0  
9.0  
10.0  
0.30  
0.35  
0.35  
0.40  
0.42  
0.45  
0.49  
0.55  
0.68  
0.75  
0.90  
1.00  
1.12  
1.19  
1.33  
0.42  
0.32  
0.32  
0.23  
0.20  
0.19  
0.23  
0.28  
0.38  
0.48  
0.52  
0.57  
0.62  
0.67  
0.69  
0.08  
0.07  
0.07  
0.06  
0.05  
0.05  
0.04  
0.03  
0.04  
0.07  
0.13  
0.25  
0.43  
0.65  
0.85  
26.23  
21.96  
21.16  
18.47  
17.18  
16.48  
15.09  
13.70  
11.85  
10.49  
9.27  
MAG  
98.80  
2
|S  
|
21  
114.10  
153.70  
171.50  
-156.70  
-133.30  
-110.70  
-89.60  
-70.80  
-54.60  
-40.80  
-10  
0
5
10  
FREQUENCY (GHz)  
15  
20  
Figure 26. MSG/MAG and |S21|  
2 vs. Frequency at 4V, 80 mA.  
8.27  
7.28  
6.66  
6.31  
Notes:  
1. The Fmin values are based on a set of 16 noise figure measurements made at 16 different impedances using an ATF NP5 test system. From these  
measurements a true Fmin is calculated. Refer to the noise parameter application section for more information.  
2. S and noise parameters are measured on a microstrip line made on 0.025 inch thick alumina carrier. The input reference plane is at the end  
of the gate lead. The output reference plane is at the end of the drain lead. The parameters include the effect of four plated through via holes  
connecting source landing pads on top of the test carrier to the microstrip ground plane on the bottom side of the carrier. Two 0.020 inch  
diameter via holes are placed within 0.010 inch from each source lead contact point, one via on each side of that point.  
13  
Noise Parameter Applications Information  
Fmin values at 2 GHz and higher are based on  
measurements while the Fmins below 2 GHz have been  
extrapolated. The Fmin values are based on a set of  
16 noise figure measurements made at 16 different  
impedances using an ATN NP5 test system. From these  
measurements, a true Fmin is calculated. Fmin represents  
the true minimum noise figure of the device when the  
deviceispresentedwithanimpedancematchingnetwork  
that transforms the source impedance, typically 50Ω, to  
an impedance represented by the reflection coefficient  
o. The designer must design a matching network that  
will present o to the device with minimal associated  
circuit losses. The noise figure of the completed amplifier  
is equal to the noise figure of the device plus the losses  
of the matching network preceding the device. The  
noise figure of the device is equal to Fmin only when the  
device is presented with o. If the reflection coefficient  
of the matching network is other than o, then the noise  
figure of the device will be greater than Fmin based on  
the following equation.  
of the matching networks are non-zero and they will  
also add to the noise figure of the device creating a  
higher amplifier noise figure. The losses of the matching  
networks are related to the Q of the components and  
associated printed circuit board loss. o is typically fairly  
low at higher frequencies and increases as frequency is  
lowered. Larger gate width devices will typically have a  
lower o as compared to narrower gate width devices.  
Typically for FETs, the higher o usually infers that an  
impedance much higher than 50Ω is required for the  
device to produce Fmin. At VHF frequencies and even  
lower L Band frequencies, the required impedance can  
be in the vicinity of several thousand ohms. Matching to  
such a high impedance requires very hi-Q components  
in order to minimize circuit losses. As an example at  
900 MHz, when airwwound coils (Q>100) are used for  
matching networks, the loss can still be up to 0.25 dB  
which will add directly to the noise figure of the device.  
Using muiltilayer molded inductors with Qs in the 30 to  
50 range results in additional loss over the airwound coil.  
Losses as high as 0.5 dB or greater add to the typical 0.15  
dB Fmin of the device creating an amplifier noise figure  
of nearly 0.65 dB. A discussion concerning calculated  
and measured circuit losses and their effect on amplifier  
noise figure is covered in Avago Application 1085.  
2
NF = Fmin + 4 Rn  
Zo  
|
s  
o |  
(|1 +  
o|2)(1s|2)  
Where Rn/Zo is the normalized noise resistance, o is  
the optimum reflection coefficient required to produce  
Fmin and s is the reflection coefficient of the source  
impedance actually presented to the device. The losses  
Reliability Data  
Nominal Failures per million (FPM)  
for different durations  
90% confidence Failures per million (FPM)  
for different durations  
Channel  
Temperature  
(oC)  
(FITs)  
1000  
hours  
1 year  
5 year  
10 year  
30 year  
(FITs)  
1000  
hours  
1 year  
5 year  
10 year  
30 year  
100  
125  
140  
150  
160  
<0.1  
<0.1  
<0.1  
<0.1  
<0.1  
<0.1  
<0.1  
<0.1  
<0.1  
<0.1  
<0.1  
4400  
<0.1  
<0.1  
<0.1  
2
<0.1  
<0.1  
<0.1  
140  
<0.1  
<0.1  
160  
<0.1  
<0.1  
<0.1  
<0.1  
<0.1  
21  
<0.1  
<0.1  
<0.1  
0.3  
<0.1  
<0.1  
6
<0.1  
<0.1  
160  
<0.1  
11  
9.3K  
131K  
520K  
1000K  
26K  
780  
24K  
590K  
8800  
120K  
850K  
920  
450K  
21K  
370K  
1000K  
67  
180  
830K  
53K  
NOT  
recommended  
Predicted failures with temperature extrapolated from failure distribution and activation energy data of higher temperature  
operational life STRIFE of PHEMT process  
14  
ATF-33143 Die Model  
Statz Model  
MESFETM1  
NFET=yes  
PFET=no  
Vto=–0.95  
Beta=0.48  
Lambda=0.09  
Alpha=4  
B=0.8  
Cgs=1.6 pF  
Gdcap=3  
Cgd=0.32 pF  
Rgd=  
Rc=62.5  
Gsfwd=1  
Gsrev=0  
Gdfwd=1  
Gdrev=0  
Vjr=1  
Taumd1=no  
Fnc=1E6  
R=0.17  
C=0.2  
Tqm=  
P=0.65  
Vmax=  
wVgfwd=  
wBvgs=  
Fc=  
Is=1 nA  
Ir=1 nA  
Imax=0.1  
Xti=  
Tnom=27  
Idstc=  
Rd=.125  
wBvgd=  
wBvds=  
Rg=1  
Vbi=0.7  
Tau=  
Rs=0.0625  
Ld=0.00375 nH  
Lg-0.00375 nH  
Ls=0.00125 nH  
Cds=0.08 pF  
Crf=0.1  
wldsmax=  
wPmax=  
Al lParams=  
N=  
Betatce=  
Delta1=0.2  
Delta2=  
Eg=  
Vbr=  
Vtotc=  
Rin=  
Gscap=3  
This model can be used as a design tool. It has been tested  
on MDS for various specifications. However, for more precise  
and accurate design, please refer to the measured data in  
this data sheet. For future improvements Avago reserves  
the right to change these models without prior notice.  
ATF-33143 Model  
INSIDE Package  
Var  
VIA2  
VAR  
Ean  
V3  
VAR1  
TLINP  
TLINP  
D=20.0 mil  
H=25.0 mil  
T=0.15 mil  
Rho=1.0  
W=40.0 mil  
K=5  
TL1  
TL2  
Z2=85  
Z1=30  
Z=Z2/2 Ohm  
L=20 0 mil  
K=K  
Z=Z2/2 Ohm  
L=20 0 mil  
K=K  
C
A=0.0000  
F=1 GHz  
TanD=0.001  
A=0.0000  
F=1 GHz  
TanD=0.001  
C1  
GATE  
SOURCE  
C=0.1 pF  
L
L
Port  
TLINP  
TL7  
TLINP  
TL8  
TLINP  
TLINP  
Port  
S2  
L6  
L1  
G
TL4  
TL3  
L=0.2 nH  
R=0.001  
L=0.6 nH  
R=0.001  
Num=1  
Z=Z2/2 Ohm Z=Z1 Ohm  
VIA2  
VIA2  
Z=Z1 Ohm  
L=15 mil  
K=1  
Z=Z2 Ohm  
L=25 mil  
K=K  
Num=4  
L=5.0 mil  
K=K  
L=15 mil  
K=1  
V1  
V4  
GaAsFET  
D=20 mil  
H=25.0 mil  
T=0.15 mil  
Rho=1.0  
W=40 mil  
D=20.0 mil  
H=25.0 mil  
T=0.15 mil  
Rho=1.0  
W=40.0 mil  
C
A=0.0000  
F=1 GHz  
A=0.0000  
F=1 GHz  
FET1  
C2  
A=0.000  
F=1 GHz  
A=0.000  
F=1 GHz  
Model=MESFETN1  
Mode=nonlinear  
C=0.11 pF  
TanD=0.001 TanD=0.001  
DRAIN  
TanD=0.001 TanD=0.001  
SOURCE  
L
TLINP  
TLINP  
Port  
D
L7  
TL5  
TL6  
C=0.6 nH  
R=0.001  
L
Port  
S1  
TLINPTL9  
Z=Z2 Ohm  
L=10.0 mil  
K=K  
Z=Z2 Ohm  
L=26.0 mil  
K=K  
Z=Z1 Ohm  
L=15 mil  
K=1  
TLINP  
Num=4  
L4  
MSub  
TL10  
VIA2  
L=0.2 nH  
R=0.001  
Num=2  
Z=Z1 Ohm  
L=15 mil  
K=1  
MSUB  
V2  
A=0.0000  
F=1 GHz  
A=0.0000  
F=1 GHz  
MSub1  
H=25.0 mil  
Er=9.6  
D=20.0 mil  
H=25.0 mil  
T=0.15 mil  
Rho=1.0  
W=40.0 mil  
A=0.000  
F=1 GHz  
TanD=0.001  
TanD=0.001 TanD=0.001  
A=0.000  
F=1 GHz  
TanD=0.001  
Mur=1  
Cond=1.0E+50  
Hu=3.9e+0.34 mil  
T=0.15 mil  
TanD=D  
Rough=D mil  
15  
Part Number Ordering Information  
No. of  
Part Number  
ATF-33143-TR1G  
ATF-33143-TR2G  
ATF-33143-BLKG  
Devices  
3000  
10000  
100  
Container  
7Reel  
13Reel  
antistatic bag  
Package Dimensions  
SC-70 4L/SOT-343  
Recommended PCB Pad Layout for  
Avago’s SC70 4L/SOT-343 Products  
1.30 (.051)  
BSC  
1.30  
(0.051)  
1.00  
(0.039)  
HE  
E
2.00  
(0.079)  
0.60  
(0.024)  
1.15 (.045) BSC  
0.9  
(0.035)  
b1  
1.15  
D
(0.045)  
mm  
(inches)  
Dimensions in  
A
A2  
A1  
b
C
L
DIMENSIONS (mm)  
SYMBOL  
E
D
HE  
A
A2  
A1  
b
MIN.  
1.15  
1.85  
1.80  
0.80  
0.80  
0.00  
0.15  
0.55  
0.10  
0.10  
MAX.  
1.35  
2.25  
2.40  
1.10  
1.00  
0.10  
0.40  
0.70  
0.20  
0.46  
NOTES:  
1. All dimensions are in mm.  
2. Dimensions are inclusive of plating.  
3. Dimensions are exclusive of mold flash & metal burr.  
4. All specifications comply to EIAJ SC70.  
5. Die is facing up for mold and facing down for trim/form,  
ie: reverse trim/form.  
b1  
c
L
6. Package surface to be mirror finish.  
16  
Device Orientation  
REEL  
TOP VIEW  
4 mm  
END VIEW  
CARRIER  
TAPE  
8 mm  
3Px  
3Px  
3Px  
3Px  
USER  
FEED  
DIRECTION  
COVER TAPE  
Tape Dimensions and Product Orientation For Outline 4T  
P
2
P
P
D
o
E
F
W
C
D
1
t (CARRIER TAPE THICKNESS)  
1
T (COVER TAPE THICKNESS)  
t
K
o
10 MAX.  
10 MAX.  
A
B
o
o
DESCRIPTION  
SYMBOL  
SIZE (mm)  
2.40 0.10  
2.40 0.10  
1.20 0.10  
4.00 0.10  
1.00 + 0.25  
SIZE (INCHES)  
CAVITY  
LENGTH  
WIDTH  
DEPTH  
PITCH  
A
B
K
P
0.094 0.004  
0.094 0.004  
0.047 0.004  
0.157 0.004  
0.039 + 0.010  
o
o
o
BOTTOM HOLE DIAMETER  
D
1
PERFORATION  
DIAMETER  
PITCH  
POSITION  
D
1.55 0.10  
4.00 0.10  
1.75 0.10  
0.061 + 0.002  
0.157 0.004  
0.069 0.004  
P
o
E
CARRIER TAPE  
COVER TAPE  
DISTANCE  
WIDTH  
THICKNESS  
W
8.00 + 0.30 - 0.10 0.315 + 0.012  
t
0.254 0.02  
0.0100 0.0008  
1
WIDTH  
TAPE THICKNESS  
C
T
5.40 0.10  
0.062 0.001  
0.205 + 0.004  
0.0025 0.0004  
t
CAVITY TO PERFORATION  
(WIDTH DIRECTION)  
F
3.50 0.05  
0.138 0.002  
CAVITY TO PERFORATION  
(LENGTH DIRECTION)  
P
2
2.00 0.05  
0.079 0.002  
For product information and a complete list of distributors, please go to our web site: www.avagotech.com  
Avago, Avago Technologies, and the A logo are trademarks of Avago Technologies in the United States and other countries.  
Data subject to change. Copyright © 2005-2012 Avago Technologies. All rights reserved. Obsoletes 5989-3747EN  
AV02-1442EN - June 8, 2012  

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