Zero-Bias Offsets in the Low-Temperature Dark Current of Quantum-Well Infrared Photodetectors

Abstract

Quantum-well infrared photodetectors (QWIPs) have potential applicability in many remote-sensing applications, even in the space environment where low background fluxes are involved. In this environment, the detector arrays may need to be operated at temperatures lower then 77 K. At these temperatures, tunneling mechanisms such as Fowler-Nordheim and trap-assisted tunneling could dominate the dark current. The device resistance, which is bias-dependent, increases by several orders of magnitude at these temperatures and may pose a problem. The author have seen offsets in the current-versus-voltage (I-V) characteristics (nonzero current at zero bias not associated with dopant migration) which could impair the compatibility of a QWIP array with a readout circuit. They propose that these offsets are due to an RC time-constant effect. They further propose that the resistance in this time constant is due to tunneling mechanisms (and not due to contact resistance), which in turn are structure- and bias-dependent. They discuss their observations and present a circuit model of a QWIP that explains these observations nearly completely.

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Document Details

Document Type
Technical Report
Publication Date
Aug 01, 1999
Accession Number
ADA429637

Entities

People

  • Anjali Singh
  • D. A. Cardimona

Organizations

  • Air Force Research Laboratory

Tags

Communities of Interest

  • Advanced Electronics

DTIC Thesaurus Topics

  • Air Force Research Laboratories
  • Band Structures
  • Chemical Vapor Deposition
  • Circuit Analysis
  • Detection
  • Detectors
  • Engineering
  • Experimental Data
  • First Order Circuits
  • Low Temperature
  • Observation
  • Photodetectors
  • Quantum Tunneling
  • Quantum Wells
  • Remote Sensing
  • Resistance
  • Tunneling

Readers

  • Electrical Engineering
  • Semiconductor Device Technology
  • Systems Analysis and Design

Technology Areas

  • Quantum Computing
  • Space
  • Space - Hall-Effect Thruster