GaN HEMT Reliability

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GaN HEMT Reliability J. A. del Alamo and J. Joh Microsystems Technology Laboratories, MIT ESREF 2009 Arcachon, Oct. 5-9, 2009 Acknowledgements: ARL (DARPA-WBGS program), ONR (DRIFT-MURI program) Jose Jimenez, Sefa Demirtas 1

1. Introduction: GaN Reliability GaN HEMT: commercial technology since 2005 Great recent strides in reliability: MTTF=10 7 h at 150 C and 40 V demonstrated [Jimenez, IRPS 2008] Unique issues about GaN HEMT reliability: No native substrate (use SiC, Si, sapphire) mismatch defects High-voltage operation very high electric fields (~10 7 V/cm) Strong piezoelectric materials: high electric field high mechanical stress Electron channel charge set by polarization, not dopants Work to do before demonstrating consistent, reproducible reliability with solid understanding behind: When will we be able to put GaN in space? 2

Outline 1. Introduction 2. Experimental 3. Results 4. Hypothesis for high-voltage degradation mechanism: Defect formation through inverse piezoelectric effect 5. Discussion 6. Conclusions 3

2. Experimental GaN HEMT Reliability Test Chip 3.25 x 3.175 mm2 DC and mmw HEMTs HEMTs with different dimensions (Lrd, Lrs, Lg, Wg, #fingers) HEMTs with different orientations (0, 30o, 60o, 90o) TLM s, side-gate FET, FATFET Most devices completed before vias Implemented by BAE, TriQuint and Nitronex with own design rules 4

DC Stress Experiments START Characterization I Dmax, R S, R D, I Goff, V T Trapping Analysis Electrical Stress V DS, V GS (or I D ) 5

Characterization Suite Comprehensive, three sets of measurements: Coarse characterization: basic device parameters Fine characterization: + complete set of I-V characteristics (output, transfer, gate, subthreshold, kink) Trap analysis: transient analysis under various pulsing conditions Fast: Coarse characterization: <20 secs Fine characterization: <1 min Trap analysis: <10 min Frequent: Coarse characterization: every 1-2 mins Fine characterization, trap analysis: before, after, at key points Benign : 100 executions to produce change <2% change in any extracted parameter 6

DC Stress Schemes Stress-recovery experiments: to study trapping behavior Step-stress experiments: to study a variety of conditions in a single device (for improved experimental efficiency) Step-stress-recovery experiments: to study trap formation under different conditions in a single device 7

Electrical Stress Bias Points Hot electrons! 8

Typical GaN HEMT Source Gate Drain GaN Cap AlGaN GaN SiN 2DEG Typical values: t = 13-18 nm x = 25-30% SiC Substrate Standard device with integrated field plate : L G =0.25 um, W=4x100 um f T =40 GHz, I Dmax =1.2 A/mm P out =8 W/mm, PAE=60% @ 10 GHz, V D =40 V Test device: W=2x25 um 9

3. Results: V DS =0 Degradation V DS =0 step-stress; V DG : 10 to 50 V, 1 V/step, 1 min/step I Dmax I Dmax R ON g m 10

V DS =0 Degradation V DS =0 step-stress; V DG : 10 to 50 V, 1 V/step, 1 min/step I Goff I Gon I Doff I Goff I Gon 11

V DS =0 Degradation Joh, EDL 2008 Critical voltage for degradation: At V crit 21 V, I Goff increases ~100X, I Dmax, R S, R D start degrading 12

V DS =0 Degradation V crit At V crit 21 V, I gstress <10 ma/mm self-heating, hot electrons not responsible for V crit degradation 13

OFF-state Degradation OFF-state step-stress: V GS =- 5 V; V DS : 5 to 45 V, 1 V/step, 1 min/step; Critical behavior, but V crit 34 V V crit depends on detailed bias R S does not degrade I GDoff, I GSoff unchanged Drain side degrades, source side intact 14

High-Power Degradation High-power step-stress (fixed I Dstress ); V DS : 5 to 40 V, 1 V/step, 1 min/step Critical behavior, but I Dstress V crit Joh, IEDM 2007 Current is not accelerating factor 15

Trapping in stressed devices V DS =0 stress-recovery experiment; V GS =-40 V (beyond V crit ) Joh, IEDM 2007 I G follows same trapping behavior as I D common physical origin for I G and I D degradation In recovery phase: I Dmax, I Goff trapped electrons block I G I Gon steady traps not accessible from channel? 16

Are traps also generated at V crit? V DS =0 step-stress-recovery experiment with diagnostic pulse 10 min step, 5 min recovery, 2.5 V/step Under light to speed up recovery Joh, IEDM 2006 10 V diagnostic pulse 17

Trap density vs. damage in GaN HEMT Joh, IEDM 2006 V crit : onset of I G, I D, R S, R D degradation and trap formation 18

Other Reports of Critical Voltage Behavior V crit =30-60 V; Ivo, IRPS 2009 GaN HEMT on Si, V crit =10-75 V Demirtas, ROCS 2009 V crit =10-80 V; Zanoni, EDL 2009 19

4. Hypothesis for high-voltage degradation mechanism 1. Defects in AlGaN provide path for reverse I G (I Goff ) electron trapping n s I Dmax, R D transient effects additional non-transient degradation Φ bi High V DG defect state AlGaN GaN E C E F 20

Hypothesis for high-voltage degradation mechanism 2. Defects originate from excessive mechanical stress introduced by high electric field through inverse piezoelectric effect concentrated at gate edge builds on top of lattice mismatch stress between AlGaN and GaN when elastic energy density in AlGaN exceeds critical value 21

Role of V GS OFF-state step-stress experiments at different V GS : Joh, IEDM 2007 High-field on source side adds to stress on drain side V GS V crit 22

Role of Gate Length V DS =0 step-stress experiments for different L G Joh, IEDM 2007 L g less cumulative stress at edges L G V crit 23

Role of Mechanical Strain V DS =0 step stress Joh, IEDM 2007 External tensile strain V crit reveals mechanical origin of degradation 24

Crack and pits in stressed GaN HEMTs ON-state degradation at 40 V, I D =250 ma/mm, T a =112 C Chowdhury, EDL 2008 (a) (b) Physical degradation correlates with electrical degradation (c)

Other observations of damage at edges of gate V DS =0 Zanoni, EDL 2009 Gate current degradation correlates with elecroluminescence from gate edges 26

5. First-order model for V crit Key assumption: at V crit, elastic energy density in AlGaN reaches critical value Electrical model: 2D electrostatic simulator (Silvaco Atlas) Mechanical model: analytical formulation of stress and elastic energy vs. electric field Joh, ROCS 2009 Planar stress linear on vertical electric field Elastic energy density superlinear on vertical electric field 27

First-order model for V crit Example: 16 nm thick AlGaN with x=28% V crit condition in OFF-state (V GS =-5 V, V DS =33 V) Vertical electric field Elastic energy density Large peak of electric field and elastic energy density under gate edge on drain side Joh, ROCS 2009 28

Elastic energy density in AlGaN vs. V DG Joh, ROCS 2009 W crit due to mismatch W crit corresponding to V crit consistent with value for onset of relaxation of AlGaN/GaN heterostructures 29

Impact of AlGaN composition on V crit Joh, ROCS 2009 W = YS 2 1 h V GS =-5 V x(aln) initial elastic energy V crit 30

Consequences: HEMT reliability improved if 1. Elastic energy density in AlGaN barrier is minimized: Thinner AlGaN barrier [Lee 2005] AlGaN with lower AlN composition [Gotthold 2004, Valizadeh 2005, Jimenez 2009] Al 0.32 Ga 0.68 N t ins =14 nm 10 40 V, T j =355 C t ins =18 nm t ins =26 nm t ins =21 nm I DMax Degradation (%) 0-10 -20-30 25% lower Al Standard -40 0 100 200 300 400 500 600 Time (hours) Lee, TED 2005 Jimenez, TWHM 2009 31

1. Elastic energy density in AlGaN barrier is minimized (cont.): AlGaN buffer layer [Joh 2006] No AlN spacer [ref?] Power Degradation (db) 0.2 0.0-0.2-0.4-0.6-0.8-1.0 Baseline AlGaN Buffer A3-1.2-1.4 A1 0 5 10 15 Time (h) Joh, IEDM 2006 32

Consequences: HEMT reliability improved if 2. AlGaN barrier is mechanically strengthened: GaN cap [Gotthold 2004, Ivo 2009, Jimenez 2009] SiN passivation [Mittereder 2003, Edwards 2005, Derluyn 2005, Marcon 2009] Jimenez, TWHM 2009 33

Consequences: HEMT reliability improved if 3. Electric field across AlGaN at gate edge is minimized: Field plate [Lee 2003, Jimenez 2006] Longer gate-drain gap [Valizadeh 2005] Add GaN cap [Ivo 2009, Ohki 2009] Rounded gate edge [ref?] Jimenez, ROCS 2006 Ohki, IRPS 2009 34

Many unknowns What is the detailed nature of the defects at the gate edge? Crack? Metal diffusion down crack? Aggregation of dislocations? Other crystalline defects Role of stress gradient? Role of time? Role of temperature? Hot electron damage in high-power state? Are these mechanisms relevant under large RF drive? Why spatial variations? Role of buffer? Role of surface and surface treatments? 35

The surface matters Surface treatments prior to ohmic metal deposition and gate evaporation impact reliability Jimenez, TWHM 2009 36

6. Conclusions Unique degradation aspects of AlGaN/GaN HEMTs with relevance to degradation Need fundamental research to provide understanding Many opportunities to improve reliability Not obvious today how to accelerate degradation to provide accurate estimation of MTTF Optimistic about long-term prospects of reliable GaN HEMTs 37

More materials 38

V DS =0 Degradation V DS =0 step-stress; V DG : 10 to 50 V, 1 V/step, 1 min/step Joh, IEDM 2007 E a (I Goff ) E a (I Gon ) unchanged 39