Latchup Immunity in High Temperature Bulk CMOS Devices

Similar documents
Using HARDSIL to minimize the impact of extreme temperature on CMOS integrated circuits. VORAGO TECHNOLOGIES Austin, Texas

CSE/EE 462: VLSI Design Fall The CMOS Fabrication Process and Design Rules. Silicon Wafer. ND Multi-Project Reticle: Rocket Chip.

Report to Congress Aviation Security Aircraft Hardening Program

When most people build their avionics package,

FLIGHT PATH FOR THE FUTURE OF MOBILITY

Model Crosspoint Matrix

Ordnance Component Dynamic Test Requirements: Observations, Challenges, Recommended Investigation

INTERNATIONAL STANDARD

Implementation challenges for Flight Procedures

Model Number Structure

Multi/many core in Avionics Systems

D DAVID PUBLISHING. Development and Achievement of the T-50 Flight Control s Consolidated OFP. 1. Introduction. 2. Consolidated OFP s Needs

RNP AR APCH Approvals: An Operator s Perspective

In-Flight Entertainment and Connectivity

Applicability / Compatibility of STPA with FAA Regulations & Guidance. First STAMP/STPA Workshop. Federal Aviation Administration

Tactical Assault Ladder

SMV512K32-DB1F0E 16MB SRAM Datasheet

Hiway Gateway Specification and Technical Data

Since the voltage was bad at the power pedestal, the problem was not with the motorhome.

THE SHIFTING LANDSCAPE for THE MAINTENANCE, REPAIR AND OVERHAUL MARKET

Monitoring & Control Tim Stevenson Yogesh Wadadekar

FC-0004 P a g e 1 Rev. 0

Progressive Technology Facilitates Ground-To-Flight-Deck Connectivity

Tradition and innovation

A New Way to Work in the ERCOT Market

The organisation of the Airbus. A330/340 flight control system. Ian Sommerville 2001 Airbus flight control system Slide 1

HARD. Preventing. Nosegear Touchdowns

Gold Coast: Modelled Future PIA Queensland Awards for Planning Excellence 2014 Nomination under Cutting Edge Research category

Driving STM32 to success STM32 services for sophisticated embedded applications

HEATHROW COMMUNITY NOISE FORUM. Sunninghill flight path analysis report February 2016

Reliability of Conformal Coated Surface Mount Parts

All-Weather Operations Training Programme

SYSTEM DEVELOPMENT AND FLIGHT TEST SOLUTIONS

NEXTT. Anne Carnall Program Manager, Future Airports. 12 December 2018

Special edition paper Development of a Crew Schedule Data Transfer System

General-Use Auto-Tuning HPX-T Series

PERFORMANCE MEASURE INFORMATION SHEET #16

Successful Return to Flight of the H-IIA Launch Vehicle

BILFINGER SE NUCLEAR ENERGY PROJECTS: WE MAKE IT WORK FROM ENGINEERING AND TECHNOLOGY TO FABRICATION, CONSTRUCTION AND SERVICES

NextGen: New Technology for Improved Noise Mitigation Efforts: DFW RNAV Departure Procedures

RNP AR and Air Traffic Management

ultimate traffic Live User Guide

Cessna Corvalis TT x. INTRINZIC TM Flight Deck powered by Garmin

MONTEREY REGIONAL AIRPORT MASTER PLAN TOPICAL QUESTIONS FROM THE PLANNING ADVISORY COMMITTEE AND TOPICAL RESPONSES

2017 Digital Grid Customer Summit Session Abstracts

Multicore Processing in the Avionics Industry Needs and Concerns April 21, 2017 Greg Arundale Rockwell Collins

AWNING CONTROL KIT 98GCK-33B

SLIDING WINDOW & DOOR LOCK

Captain Jeff Martin Senior Director Flight Operations Southwest Airlines

Appendix B Ultimate Airport Capacity and Delay Simulation Modeling Analysis

Department of Defense DIRECTIVE

IATA Air Carrier Self Audit Checklist Analysis Questionnaire

Rethink Convention. LINEAGE 1000E

The Standard of Excellence in aircraft charter. Stratos Jet Charters, Inc

Helicopter Performance. Performance Class 2 - The Concept. Jim Lyons

Coating & Converting Equipment

(ii) Weight. Maximum gross weight for all tests, except where otherwise described in subparagraph (iii) below.

A Survey of Time and Space Partitioning for Space Avionics

Fly at the speed of ingenuity on your Learjet 85

Safety insulation transformers for SmartPower controller family

Amendment Docket No. FAA ; Directorate Identifier 2002-NM-12-AD

COMMUNITY NOISE MITIGATION SUGGESTIONS

Executive Summary. MASTER PLAN UPDATE Fort Collins-Loveland Municipal Airport

Unmanned Systems Certification

B 270 Superwite D Requirements deviating from these specifications must be defined in writing in a customer agreement.

VAR-501-WECC-3 Power System Stabilizer. A. Introduction

Coating & Converting Equipment

Roadmapping Breakout Session Overview

Program Manual. January 1, EarthCraft House Single Family Program. Viridiant 1431 West Main Street Richmond, VA

AAAE Rates and Charges Workshop Air Service Incentive Programs. Thomas R. Devine KAPLAN KIRSCH & ROCKWELL LLP October 2, 2012

Feasibility of Battery Backup for Flight Recorders

PERFORMANCE REPORT NOVEMBER 2017

TruPunch 1000 and TruMatic 1000 fiber. The first machine concept that grows with you. Machine tools/power tools Laser technology/electronics

Engineering Design Assurance Test Report ( S )

Thales on the Civil Aerospace market

1.231J/16.781J/ESD.224J Airport Systems Fall Security and BHS. Amedeo R. Odoni. Massachusetts Institute of Technology.

The Past, Present, and Future of Nortek and Glider Measurements

Leader/Follower Static Pairwise (RECAT Phase II) RECATEGORIZATION WORKSHOP June 20, 2011

SuperB IFR electronics: update. I SuperB Collab. Meeting QMUL Sep A.Cotta Ramusino for INFN-FE/Dip.Fisica UNIFE

Helicopter Vector IFR

10 A at 100 to 240 VAC. G3NE-220T-US (20 A at 75 to 264 VAC) 5 A at 100 to 240 VAC

INTERNAL FLOATING ROOF

AIRBUS Generic Flight Test Installation

LUXEON Rebel PLUS Freedom From Binning

Pyrolytic Graphite Sheet

Table of Contents. DS107 LUXEON Rebel PLUS Product Datasheet Lumileds Holding B.V. All rights reserved.

Materna Integrated Passenger Services (Materna ips)

ACAS on VLJs and LJs Assessment of safety Level (AVAL) Outcomes of the AVAL study (presented by Thierry Arino, Egis Avia)

B GEORGIA INFRASTRUCTURE REPORT CARD AVIATION RECOMMENDATIONS DEFINITION OF THE ISSUE. Plan and Fund for the Future:

WE BRING YOU THE LUXURY OF ROOM TO SPARE. MAKE OF IT WHAT YOU WILL.

Wrapper Instruction Register (WIR) Specifications

AASHTO AS Presented to AASHTO T 8, June 13, 2017

National Park Service Wilderness Action Plan

Electronic visibility via ADS-B for small aircraft. John Korna, NATS

Engineering Design Assurance Test Report ( S )

BIG DATA, HAPPY GUESTS: USING ANALYTICS TO ENHANCE HOTEL OPERATIONS

Real-time route planning streamlines onboard operations, reduces fuel burn and delays, and improves on-time performance.

Capacity kw. Thermal turndown from specified maximum capacity 8:1 8:1

HOTEL ROOM MANAGEMENT SYSTEM OVERVIEW

How a global corporation can benefit from the international equivalence of national measurement standards

Transcription:

Latchup Immunity in High Temperature Bulk CMOS Devices R. Lowther, W. Morris, D. Gifford, D. Duff, R. Fuller, J. Salzman* Silicon Space Technology, Inc. 804 Las Cimas Parkway, Suite 140 Austin, TX 78746 USA Email: dduff@siliconspacetech.com *Texas Instruments, Dallas, TX ABSTRACT High density, low power 180nm and 130nm CMOS SRAMs have been manufactured on bulk silicon wafers using a modified CMOS commercial process that hardens the junction isolation and has demonstrated latchup immunity at temperatures >200 C. TCAD simulations confirmed by high temperature testing indicate that a latch up free performance of SRAMs manufactured on bulk silicon modified by the HardSIL TM technology will easily extrapolate to 250 C. These process modifications result in significantly more robust CMOS circuits making them more suitable for highly reliable operations in extreme environments such as radiation and high temperature. The unique capability of HardSIL TM technology to enhance existing IC products has demonstrated excellent results with several commercial circuits. This new approach enables the conversion of commercial off the shelf (COTS) circuits to hardened hi-rel commercial circuits with dramatically improved survivability to either radiation or high temperatures. Latchup immunity has been demonstrated on two high-density bulk silicon CMOS SRAMs: a 16Mbit asynchronous SRAM manufactured at the 180nm design node and an 8Mbit dual port synchronous SRAM manufactured at 130nm. Both parts were produced in a high-volume, low-defect commercial CMOS fabrication facility in the USA. The SRAM parts were packaged in ceramic packages and characterized at temperatures ranging from 25 C to 225 C. Characterization data indicates both excellent static leakage and dynamic circuit performance for both SRAMs at these elevated temperatures. Device test structures designed with typical layout spacing rules were evaluated to quantify latchup and isolate the various leakage mechanisms. Detailed results for these test structures are presented and compared to the SRAMs using the modified HardSIL TM process. INTRODUCTION Multiple high reliability or mission critical electronic market segments including oil and gas exploration and production, aerospace, automotive, medical devices, and energy generation rely on sophisticated integrated circuits which are increasingly needed to operate in higher temperature environments. Significant gaps in multiple electronic component categories still persist for these high temperature market segments some six years after conducting an initial survey [1]. High temperature electronic applications require unique technical solutions and design considerations for survivability and for complying with other critical performance metrics such as low operating power budgets and latch-up immunity. The limitations of bulk silicon CMOS technology for high temperature operation have been reviewed previously [2, 3, 4, 5]. These limitations, namely latchup and excessive leakage, have been broadly verified relegating bulk CMOS devices to temperature operation typically below ~100 C. As a result, alternative materials such as silicon on insulator (SOI) and silicon carbide (SiC) have been explored and successfully deployed for elevated temperature applications [2, 6, 7]. While offering the fundamental advantage of latch-up immunity at elevated temperatures, SOI- and SiC-based designs suffer from the limited IP portfolio of parts, and when available, are generally much larger geometry devices. This precludes the use of most commercially available, high performance CMOS circuits; circuits highly desirable by engineers who seek increased processing power, memory, etc. 1

While these high-performance bulk CMOS ICs are abundantly available, these COTS devices are limited to temperature operation <85 C and are typically not suitable for high temperature environments such as down hole drilling (DHD). However, complex engineering workarounds for certain critical high temperature applications have been developed including extensive up-screening and testing, specialized packaging, and localized cooling. These factors, coupled with the inherent device physics limitations of the isolation properties of bulk silicon devices, limit the broad adoption of bulk CMOS devices for high temperature applications. SST has introduced a novel approach called HardSIL TM which can provide latchup immunity and excellent leakage performance in devices for high temperature applications >200 C by making astute modifications to the commercial CMOS manufacturing process to improve junction isolation. Having proven the radiation hardness of the technology across several CMOS manufacturing nodes (250nm, 180nm, and 130nm) and different bulk CMOS devices for the radiation-rich environment of space, this paper s objective is to report on the same hardening benefits of the HardSIL TM technology for high temperature environments. The technology has been successfully demonstrated in two SRAMs operating at high temperatures (>200 C) providing technical proofs for wider use of this modified bulk CMOS technology in high temperature products. Exploitation of the full portfolio of existing, high performance CMOS devices without the need for circuit redesign or the complicated engineering workarounds mentioned above would greatly enable the high temperature industry. We have chosen to develop hardened high density SRAM memories as our initial product offering due to their broad application. Many high temperature electronic applications make use of various memory devices to store the data generated, move the data from one location to another for processing, or provide configuration files for critical on-board processors. In down hole drilling applications, the need for more real-time intelligence and more comprehensive data collection is driving an unprecedented amount of enhanced processing and associated memory. To that end, this paper will focus on the high temperature characterization of our high density SRAMs and the TCAD modeling to characterize the electrical characteristics. Measurements described herein demonstrate that the HardSIL TM technology can extend bulk CMOS high temperature reliability and survivability to at least 200 C and with expected extrapolation, to 250 C or higher. CMOS LATCHUP The greatest risk for high reliability CMOS circuits is latchup. The basic switching circuit is the inverter composed from a complementary pair of MOS transistors, one NMOS and the other PMOS (Figure 1). Figure 1: CMOS inverter showing bipolar parasitics. Electrical isolation is achieved from both dielectrics and from p-n junction diodes. However, the CMOS twin well structure also contains a parasitic resistor/bipolar transistor network which can be biased into a high current, low impedance state. This state is known as latchup, and it can physically destroy the silicon integrated circuit if not properly mitigated. The network of series resistors shown in Figure 1 can allow the local potentials to stray from their intended values as defined by the electrode biases, allowing the structure to trigger into this latchup state [8, 9]. The latchup state is characterized by significant potential drops across both the Nwell and Pwell parasitic resistances, forward biasing of the emitters of both the parasitic NPN and PNP devices, and collapse of the Nwell/Pwell junction. It can be triggered by a random ionizing event such as an ion strike, or it can be caused by a voltage spike on any of the 2

electrodes. This latter path to latchup is simulated on a latchup structure shown in Figure 2. Figure 3 shows the p+ current as the p+ electrode boundary conditions are swept. Key features are the trigger current and trigger voltage as defined by the rightmost point of the trace, and the holding voltage as defined by the leftmost point on the high-current, or latched part of the trace. Increasing trigger current and increasing trigger voltage indicate decreasing probability of accidentally moving into the latchup state. A holding voltage less than the supply voltage allows the latchup state to be sustained indefinitely, and possibly destructively. Even a transient triggering event can be disruptive enough to cause the upset of a large region of CMOS circuit, compromising either memory or logic. This ability of a latchup event to spread in area is demonstrated in the next simulation. Nwell Tap Pplus p+ Nplus n+ Pwell Tap Figure 3: Latchup current vs. voltage. Figure 4 shows a simulation of two inverters after latchup was induced by tracing the right PMOS drain as described above. The current flow lines indicate both total current direction and total current density with 3% of the total current flowing between each pair of adjacent flow lines. The interesting point here is that large currents flow not only on the right side of the simulation, but also on the left side, to where the latchup event has spread via collapse of the well junction. Figure 5 shows this evolution of the currents for each of the silicon nodes vs. PdrainR (drain of PFET on right side) voltage. Simulations on the HardSIL TM variant of this 2-inverter structure show no sign of latchup up to five volts on PdrainR (Figure 6). Left NFET Left PFET Nwell Tap Right PFET Right NFET Pwell Tap Figure 2: Latchup test structure showing the parasitic resistor/bipolar transistor network. Figure 4: Device simulation of two inverters in a latched state. The thick lines indicate junctions, and the thin lines indicate current contours. I(Pdrain) (Arbitrary Units) Holding Voltage Trigger Voltage, Trigger Current VDD Figure 5: Terminal currents (arbitrary units) in the two- inverter simulation (control). The boundary conditions of PdrainR are stepped. 3

I(p+) (Amps) 0.1 0.09 0.08 0.07 0.06 0.05 0.04 0.03 0.02 Control @25C Control @85C Control @125C Control @150C Control @175C Control @200C HardSIL @25C HardSIL @85C HardSIL @125C HardSIL @150C HardSIL @175C HardSIL @200C HardSIL Figure 6: Terminal currents (arbitrary units) in the two- inverter simulation (HardSIL TM ). LATCHUP MEASUREMENTS If the trigger and holding voltages can be made so high that devices would first break down through other mechanisms such as gate oxide failure, then for all practical purposes the latchup state does not exist. With the high integration at these technology nodes, this is the simplest way to ensure that latchup cannot occur anywhere on the circuit. Latchup structures in the 130nm technology node were drawn and tested. The measured structures are the same as shown in Figure 2, with the minimum spacing rules, and a width of 20µm in the z- direction. By applying a voltage sweep at the P+ diffusion the PNP devices is activated and latchup traces were taken for both the control and HardSIL TM cases at temperatures up to 200 C (Figure 7). The control case went into a latched state at all temperatures; with decreasing trigger current, trigger voltage, and holding voltage as the temperature was increased. At 175 C and above, the holding voltage has dropped below the supply voltage of 1.5 V, indicating that if the overvoltage stimulus was removed the latched state could be sustained. However, none of the HardSIL TM cases latched, nor was there any indication that they would have even if higher temperatures had been tested beyond the equipment test limit of 200 C. In fact, the simulations of these same structures, which agree well with the measurements of Figure 7, indicate no sign of latchup up to 275 C. 0.01 0 0 0.5 1 1.5 2 2.5 3 3.5 V(p+) (Volts) Figure 7: Measured currents from a latchup test core devices. The temperature is stepped to 200 C for both the control and HardSIL TM cases. This same structure, with the minimum Nwell edge spacing ground rules for core devices, was further stressed by increasing the V DD voltage from 1.5V to 3.3V as is used in the I/O devices. Normally, I/O devices need about three times the minimum allowed spacing rules to the Nwell edge to prevent latchup. As seen from Figure 8, latchup occurs in the control case and is prevented in the HardSIL TM case. This suggests that the HardSIL TM technology can be used to improve the trade-off between layout ground rules/total area and the assurance of latchup prevention. Because latchup in the I/O has been a big concern historically, the approach with HardSIL TM has been to retain the established ground rules to gain the added security against latchup. 4

Ip+ (Amps) 0.08 0.07 0.06 0.05 0.04 0.03 Control @25C Control @85C Control @125C Control @150C Control @175C Control @200C HardSIL @25C HardSIL @85C HardSIL @125C HardSIL @150C HardSIL @175C HardSIL @200C 0.02 0.01 0 0 0.5 1 1.5 2 2.5 3 3.5 4 4.5 5 Vp+ (Volts) Figure 8: Measured currents from the latchup test device with V DD=3.3V. The temperature is stepped to 200 C for both the control and HardSIL TM cases. LEAKAGE There are several mechanisms through which unwanted current can leak from V DD to ground: junction leakage through the reverse-biased drains and through the reverse-biased Nwell-Psubstrate junctions, NMOS-Pwell or interdevice leakage along a shallow trench, or intradevice source-todrain leakage. The HardSIL TM process changes reduce junction leakage, particularly the Nwell- Psubstrate leakage which is reduced by more than a factor of ten at 200 C as shown in Figure 9. The Ndrain leakage is also reduced, but by a much smaller factor. However, the largest contribution to overall leakage in these highly integrated digital CMOS circuits is source-to-drain current in the CMOS transistors themselves either under the gate according to the basic subthreshold characteristics, or along the edge, assisted by charge traps in the oxide near the interface. The HardSIL TM technology has been used to specifically reduce NMOS source-drain leakage, mainly to prevent increased leakage from TID (Total Ionizing Dose) in radiation environments. As shown from measured data in Figure 10, there is also significant leakage reduction at high temperature, without radiation. Figure 9: Measured averaged Nwell- Psubstrate junction leakage currents vs. temperature ( C). The drawn Nwell area is 503 µm 2. Idrain (Amps) 1.E- 04 1.E- 05 1.E- 06 1.E- 07 1.E- 08 1.E- 09 1.E- 10 1.E- 11 1.E- 12 Control @25C Control @125C Control @200C HardSIL @25C HardSIL @125C HardSIL @200C 0 0.25 0.5 0.75 1 1.25 1.5 Vgate (Volts) Figure 10: Gate current sweeps of control and HardSIL TM NMOS core transistors (L=115nm, W=250nm) at the 130nm CMOS technology node. For example, the control and HardSIL TM I on currents at 200 C are within 3% of each other (1.16e-4 Amps and 1.13e-4 Amps respectively), yet the HardSIL TM devices have smaller I off by a factor of 4.3 (2.93e-9 Amps and 6.77e-10 Amps, respectively). SRAM HIGH TEMPERATURE TESTING Two different SRAM memory products have been fabricated with the HardSIL TM technology. A 16 5

Mbit SRAM at the 180nm technology node, and an 8 Mbit dual-port SRAM at the 130nm node. For these full parts, as opposed to structures on a test chip, full control cases were not fabricated because that would have involved expensive layout differences. This section concentrates on the performance of the HardSIL TM SRAM parts themselves. Figure 11 shows plots of I DD1 stand-by current and read current for the 16 Mbit SRAM at temperatures from 25 C to 225 C. Above 200 C, the leakage current is comparable to the read and write currents. Figure 12 shows leakage current of the 8 Mbit dual-port SRAM vs. temperatures from 25 C to 225 C. In both SRAMs, HardSIL TM acts to limit leakage and as can be seen up to 225 C, the leakage increases in a log normal fashion. Additional high temperature characterization and testing of HardSIL TM parts will continue in order to establish survivability metrics, statistically validate electrical performance, etc. Commercial off the Shelf (COTS) bulk CMOS IC s are generally not optimized for high temperature use. HardSIL TM represents a new approach to hardening the CMOS process technology used to manufacture CMOS IC s and has been proven to prevent latchup even while operating at temperatures >200 C. SOI technology has long been the incumbent solution for high temperature applications requiring latchup free performance with reduced leakage performance relative to traditional bulk CMOS. However, the results published here provide compelling evidence that HardSIL TM offers a viable high temperature alternative to SOI which would increase the availability of high performance, HT-CMOS devices due to the large IP portfolio and existing circuit designs used in COTS. Upgrading existing bulk silicon devices by manufacturing them with the HardSIL TM process will greatly expand the availability of components operating reliably at temperatures >200 C. This modified bulk CMOS process offers a new, high performance hi-rel solution with latchup immunity for T>200 and lower leakage relative to conventional bulk CMOS technology. REFERENCES [1] Normann, Randy A., First High- Temperature Electronics Products Survey 2005, Sandia Report SAND2006-1580, 2006. Figure 11: 180nm 16M SRAM SIDD1 and 5Mhz read current vs. temperature. [2] Colin Johnson and Alison Crossley, High Temperature Electronics in Geothermal Tools, HITI Final Paper, 16-17, Sept. 2010. [3] Patrick McClusky, Richard Grzybowski, Thomas Podlesak, editors, High Temperature Electronics, CRC Press, 1997. [4] B.L. Gingerich, SPE, and P.G. Brusius, Reliable Electronics for High- Temperature Downhole Applications, 1999 SPE Annual Technical Conference and Exhibition, Houston, Texas, 3-6 October 1999. Figure 12: 130nm 8M SRAM SIDD1 and 5MHz read, write currents vs. temperature. Summary [5] Pect, Micheal. The Influence of Temperature on Integrated Circuit Failure Mechanisms., Quality and Reliability Engineering International, May- June 1992, Vol. 8, No 3, pp.167-175. 6

[6] Bruce Ohme and Michael T. Johnson, Deep Trek Re- configurable Processor for Data Acquisition (RPDA), Final Report, DOE Award No.: DE- FC26-06NT42947, Sept. 2009. [9] S. Voldman, Latchup, ISBN: 987-0- 470-01642- 8, Feb. 2008. [7] L. Evans, High Temperature Electronics for Intelligent Harsh Environment Sensors, PWIG Workshop, May 2008. 8] R. Troutman, Latchup in CMOS Technology: The Problem and the Cure, Kluwer Publications, Ch. 6 and 7, 1986. 7