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J. Vac. Sci. Technol. B 30, 02B118 (2012); http://dx.doi.org/10.1116/1.3678206 (4 pages)

InAs MOS devices passivated with molecular beam epitaxy-grown Gd2O3 dielectrics

C. A. Lin1, M. L. Huang1, P.-C. Chiu2, H.-K. Lin2, J.-I. Chyi2, T. H. Chiang3, W. C. Lee3, Y. C. Chang3, Y. H. Chang3, G. J. Brown4, J. Kwo5, and M. Hong6

1Department of Physics, National Tsing Hua University, Hsinchu 30013, Taiwan
2Department of Electrical Engineering, National Central University, Jhongli 32001, Taiwan
3Department of Materials Science and Engineering, National Tsing Hua University, Hsinchu 30013, Taiwan
4Air Force Research Laboratory (AFRL), Dayton, Ohio 45433
5Center for Condensed Matter Sciences, National Taiwan University, Taipei, 10617 Taiwan
6Department of Physics and Graduate Institute of Applied Physics, National Taiwan University, Taipei, 10617 Taiwan

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(Published online 1 February 2012)

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InAs MOS devices passivated with molecular beam epitaxy (MBE)-grown Gd2O3 2–3 monolayers thick followed by an Al2O3 cap have demonstrated excellent electrical performances and interfacial properties. Band offset energies of in situ atomic-layer-deposited (ALD)-Al2O3/MBE-Gd2O3/InAs and ALD-Al2O3/InAs were determined by in situ x-ray photoelectron spectroscopy in conjunction with Fowler–Nordheim tunneling current analysis. A conduction-band offset energy (ΔEc) and a valence-band offset energy of 2.3 and 3.92 eV for ALD-Al2O3/InAs were determined, respectively. The insertion of a Gd2O3 layer increases the value of ΔEc by nearly 0.1 eV as compared to the case for Al2O3 directly deposited on InAs. The distribution of interfacial density of states (Dit) within the InAs bandgap, deduced by the conductance method at 77 K, gives a low Dit value of 1012 cm−2 eV−1 near the conduction-band edge. Moreover, with energy band engineering in the heterostructure, gate-first depletion channel InAs MOSFETs have produced drain current density of 46 μA/μm and transconductance of 17 μS/μm for 12-μm-gate-length devices at 300 K.

© 2012 American Vacuum Society

ACKNOWLEDGMENTS

The authors thank the National Science Council, Taiwan for supporting this work under Grant Nos. NSC-98-2120-M-007-002 and NSC-97-3114-M-007-001. The support from the Asian Office of Aerospace Research and Development of the U.S. Air Force is acknowledged.

Article Outline

  1. INTRODUCTION
  2. EXPERIMENT
  3. RESULTS AND DISCUSSION
  4. CONCLUSION

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1071-1023 (print)  
1520-8567 (online)

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