High Voltage DC and RF Power Reliability of GaN HEMTs J. A. del - - PowerPoint PPT Presentation

high voltage dc and rf power reliability of gan hemts
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High Voltage DC and RF Power Reliability of GaN HEMTs J. A. del - - PowerPoint PPT Presentation

High Voltage DC and RF Power Reliability of GaN HEMTs J. A. del Alamo and J. Joh* Microsystems Technology Laboratories, MIT, Cambridge, MA (USA) *presently with Texas Instruments, Dallas, TX (USA) ICNS 2011 Glasgow, July 10-15, 2011


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SLIDE 1

High‐Voltage DC and RF Power Reliability of GaN HEMTs

  • J. A. del Alamo and J. Joh*

Microsystems Technology Laboratories, MIT, Cambridge, MA (USA) *presently with Texas Instruments, Dallas, TX (USA)

ICNS 2011

Glasgow, July 10-15, 2011

Acknowledgements: ARL (DARPA-WBGS program), ONR (DRIFT-MURI program) Accel-RF Corporation

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SLIDE 2

Micovic, Cornell Conf 2010 94‐95 GHz MMIC PAs: Micovic, MTT‐S 2010

Pout>40 W/mm,

  • ver 10X GaAs!

Wu, DRC 2006

Breakthrough RF‐mmw power in GaN HEMTs

2

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SLIDE 3

3

GaN HEMTs in the field

Counter‐IED Systems (CREW) 200 W GaN HEMT for cellular base station Kawano, APMC 2005 100 mm GaN‐on‐SiC volume manufacturing Palmour, MTT‐S 2010

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SLIDE 4

Recent great strides in RF power reliability

4

28 V RF oper. life > 2 years (X‐ band, 3 dB comp., ~150oC) Kolias, MTT‐S 2010 MTTF=1x107 h at 47 V (C‐ band, 5 dB comp., ~150oC) Yamasaki, MTT‐S 2010 MTTF=7x107 h at 28 V (40 GHz, 1.5 dB comp., ~150oC) Heying, MTT‐S 2010

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SLIDE 5
  • In general:

– RF stress  Pout↓, Gain↓, IDmax↓, |IG|↑, VT shift, dispersion↑ – RF introduces more degradation than DC – RF stress accelerated by VDQ, Pin, Tj

Dominant degradation mechanisms under RF stress?

5

Conway, IRPS 2007; Joh, ROCS 2008, IEDM 2010, ROCS 2011; Chini, IEDM 2009

  • Indications of two competing

mechanisms:

– Trap creation and trapping? – Field‐driven structural degradation? Chini, EUMW 2009 Rozman, ROCS 2009; Chini, IEDM 2009 Dammann, IRPS 2010

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SLIDE 6

Outline

  • 1. RF power reliability concerns
  • 2. Methodology for RF reliability experiments
  • 3. Electrical and structural results
  • 4. Discussion: the role of gate placement
  • 5. Conclusions

6

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SLIDE 7

RF power reliability concerns

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OFF and semi‐ON high‐voltage DC stress : – Degradation of IDmax, RD, IGoff – VT shift – Electron trapping – Trap creation – Formation of grooves and pits under drain‐end of gate High‐power DC stress: – Not accessible to DC stress experiments – Device blows up instantly ON DC stress: – Mostly benign

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SLIDE 8

RF experiment flowchart: conventional approach

8

Limitations:

  • Bias point shifts during stress
  • Limited RF characterization
  • No DC characterization
  • No trap characterization
  • If examining different RF

conditions, RF characterization confusing START RF Stress Pout, PAE, Gain, IDQ, IGQ END

Tstress

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SLIDE 9

RF experiment flowchart: improved approach (I)

New features:

  • RF and DC characterization under

standardized conditions

  • At beginning, end and periodically

through experiment Limitations:

  • Limited characterization
  • Characterization temperature

cannot be too different from stress temperature

  • Cannot separate trapping from

“permanent” degradation

9

START RF Stress

Short Characterization (DC, RF)

End?

YES NO

Tstress Tbase

END

Short Characterization (DC, RF)

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SLIDE 10

RF experiment flowchart: improved approach (II)

New features:

  • Comprehensive DC, RF and

pulsed characterization under standardized conditions (RT)

  • At beginning, end, and during

experiment

  • Detrapping step to enable trap

characterization

10

Full Characterization (DC, RF, CC)

START RF Stress

Short Characterization (DC, RF)

Key Event?

END: detrapping + Full characterization

YES Detrapping NO

Tstress RT Tbase

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SLIDE 11

Setup for RF reliability studies

11

DC/Pulsed Characterization

‐ KeithleySources ‐ Agilent B1500A

Windows‐based PC Accel‐RF System Hardware

MIT RF/DC Characterization Suite ‐ DC FOMs ‐ Current collapse

DUT

Switching Matrix RF/DC Units Accel‐RF Software ‐ RF measurement ‐Temperature control ‐ Stressing

Tbase

Heater

Augmented with:

  • external instrumentation for DC/pulsed

characterization

  • software to control external

instrumentation and extract DC and RF FOMs Accel‐RF AARTS RF10000‐4/S system:

  • two 2‐4 GHz channels
  • two 7‐12 GHz channels
  • Max Pin=30 dBm
  • Tbase=50‐200 °C
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SLIDE 12

RF‐stress experiments

12

Full Characterization (DC, RF, CC)

START RF (DC) Stress

Short Characterization (DC, RF) Key Event?

END: detrapping + Full characterization

YES

Detrapping

NO

Tstress RT Tbase=50°C

Tbase=100°C for 30 mins – Full DC I‐V sweeps – RF power sweep @ VDS=28 V, IDQ=100 mA/mm – Current collapse (after 1” VDS=0, VGS=‐ 10 V pulse) – Room temperature – DC FOMs: IDmax, RS, RD, VT, IGoff, … – RF FOMs @ VDS=28 V, IDQ=100 mA/mm

  • Saturated conditions (Pin=23 dBm):

Pout,sat, Gsat, PAE

  • Linear conditions (Pin=10 dBm): Glin

– Every few minutes at Tbase=50°C

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SLIDE 13

5 10 15 20 25 2 4 6 8 10 12 14 10 15 20 25 30

PAE (%) Gain (dB) Pin (dBm) PAE Gain

RF stress experiments: Pin step‐stress

13

  • Motivation:

– higher Pin  larger V waveform at output

  • MMIC:

– single‐stage internally‐matched – 4x100 μm GaN HEMT (OFF-state Vcrit >60 V at RT) – Gate centered in S‐D gap

  • Step Pin stress:

– VDS = 40 V, IDQ = 100 mA/mm – Pin = 0 (DC), 1, 20‐27 dBm – 300 min stress at each step – Tstress=50 °C (Tj=110‐230°C)

VDS=40 V, IDQ=100 mA/mm Joh, ROCS 2011

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SLIDE 14

10 20 30 40 50 60 29 30 31 32 33 Time (hr) Pout (dBm) 10 20 30 40 50 60 5 10 15 20 25 30 Time (hr) Pin (dBm)

Evolution of RF stress

14

  • Pin changing  RF FOMs changing
  • Degradation apparent but not easily quantifiable

Pout Gain

Pin Pout IDQ PAE

Full Characterization (DC, RF, CC)

START RF (DC) Stress

Short Characterization (DC, RF) Key Event?

END: detrapping + Full characterization

YES

Detrapping

NO

Tstress RT Tbase=50°C

DC DC

20 40 60

  • 100

100 200 300 400 Time (hr) IDQ (mA/mm) 10 20 30 40 50 60 5 10 15 20 25 30 Time (hr) PAE (%)

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SLIDE 15

RF FOM during short characterization

15

  • Mild degradation under DC and low Pin
  • Adding RF increases degradation: Pin ↑  Pout ↓

Full Characterization (DC, RF, CC)

START RF (DC) Stress

Short Characterization (DC, RF) Key Event?

END: detrapping + Full characterization

YES

Detrapping

NO

Tstress RT Tbase=50°C Pout at Pin=23 dBm, Glin at Pin=10 dBm VDS=28 V, IDQ=100 mA/mm, Tbase=50°C

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SLIDE 16

1.E-06 1.E-05 1.E-04 1.E-03 1.E-02 1.E-01 1.E+00 1.E+01 0.8 0.9 1 1.1 1.2 1000 2000 3000 |IGoff| (mA/mm) IDmax/IDmax(0), R/R(0) Time (min)

IDmax RS RD IGoff

DC|Pin=1 20 21 22 23 24 25 26 27 dBm

DC FOM during short characterization

16

  • Mild degradation under DC and low Pin
  • At Pin=20 dBm, step degradation in IGoff
  • Beyond Pin=20 dBm, increasing degradation of IDmax and RD

Tbase=50°C

Full Characterization (DC, RF, CC)

START RF (DC) Stress

Short Characterization (DC, RF) Key Event?

END: detrapping + Full characterization

YES

Detrapping

NO

Tstress RT Tbase=50°C

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SLIDE 17

29 30 31 32 33 1 2 3 4 5 6 7 8 9 ‐10 10 20 30 Saturated Pout (dBm) Permanent IDmax Degradation (%) Current Collapse (%) Stress Input Power Pin (dBm)

Initial DC RF

Pout  Current Collapse Δ|IDmax|

Tbase=RT

DC/RF/CC full characterization

17

  • Beyond Pin=20 dBm:

― Sharp Pout degradation ― Permanent degradation of IDmax ― Increased CC  evidence of new trap creation

Full Characterization (DC, RF, CC)

START RF (DC) Stress

Short Characterization (DC, RF) Key Event?

END: detrapping + Full characterization

YES

Detrapping

NO

Tstress RT Tbase=50°C 100 °C

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SLIDE 18

Structural degradation (planar view)

  • Pit formation along drain end of gate edge
  • Similar to DC high voltage OFF‐state stress

18

SEM AFM

DC OFF‐state stress, VDG=50 V, 1000 min, ~150oC Makaram, APL 2010

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SLIDE 19

HV OFF‐state DC vs. RF power degradation

19

Similar pattern of degradation:

High V end of load line responsible for degradation

HV OFF‐state DC RF power

IDmax ↓ beyond Vcrit ↓ beyond Pin‐crit RD ↑ beyond Vcrit ↑ beyond Pin‐crit RS small increase small increase IGoff ↑ beyond Vcrit ↑ beyond Pin‐crit Current Collapse ↑ beyond Vcrit ↑ beyond Pin‐crit Permanent IDmax ↓ beyond Vcrit ↓ beyond Pin‐crit Pits under drain end of gate Yes Yes Pits under source end of gate No No

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SLIDE 20

Step Pin stress: Offset Gate

1.E-03 1.E-02 1.E-01 1.E+00 1.E+01 0.5 1 1.5 2 2.5 3 300 600 900 1200 |IGoff| (mA/mm) IDmax/IDmax(0), R/R(0) Time (min)

IDmax RS RD IGoff  Inner loop (50°C) DC RF Pin=20 23 26 dBm

13 13.5 14 14.5 15 30 30.5 31 31.5 32 32.5 300 600 900 1200 Small Signal Gain Glin (dB) Saturated Pout (dBm) Time (min)

Gain Pout

DC RF Pin=20 23 26 dBm Inner loop (50°C)

RF FOMs DC FOMs Joh, IEDM 2010

  • Increased degradation under high Pin
  • No IGoff degradation
  • Degradation of IDmax and RS, not RD

20

Offset gate devices (LGS<LGD): OFF-state Vcrit > 80 V at T=150°C

Tj~170°C by adjusting Tbase

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SLIDE 21

HV OFF‐state DC vs. RF power degradation

21

Different pattern of degradation:

High V end of load line NOT responsible for degradation

HV OFF‐state DC RF power

IDmax ↓ beyond Vcrit ↓ beyond Pin‐crit RD ↑ beyond Vcrit ↑ beyond Pin‐crit RS small increase ↑↑ beyond Pin‐crit IGoff ↑ beyond Vcrit No Current Collapse ↑ beyond Vcrit ↑ beyond Pin‐crit Permanent IDmax ↓ beyond Vcrit ↓ beyond Pin‐crit Pits under drain end of gate Yes No Pits under source end of gate No No

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SLIDE 22

High‐power pulsed stress

22

  • Pulsed stress reproduces RS degradation in offset gate device
  • No RS degradation in centered gate

1 1.1 1.2 1.3 1.4 20 40 60 80 Normalized RS, RD Stress VDS (V) Offset gate Centered gate

RS RD RD RS

1 1.1 1.2 1.3 1.4 20 40 60 80 Normalized RS, RD Stress VDS (V) Offset gate Centered gate

RS RD RD RS

100 pulses, 500 μs, 0.05% duty IDpulse=950 mA/mm

  • High‐power stress not accessible in DC  pulsed stress
  • Offset‐gate and centered‐gate devices on same wafer:

High power region of load line responsible for degradation

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SLIDE 23

Summary

  • New RF reliability testing methodology developed
  • Under RF stress, degradation worse than at DC bias

point

  • Different patterns of RF degradation observed:

– In some device designs, it reproduces HV OFF‐state DC degradation (field driven) – In other device designs, degradation pattern correlates with high‐power pulsed stress (power driven?)

 DC reliability not good predictor for RF reliability  Need for fundamental studies of RF reliability

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