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Observations in Characterizing a Commercial MNOS EEPROM for Space

This study focuses on the characterization of a Hitachi HN58C1001 MNOS EEPROM for space applications, including data retention lifetime, impact of TID on data retention, and worst-case test parameters. The results show no significant degradation in performance after TID irradiation and provide insights into the time-to-failure and intermittent readout failures.

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Observations in Characterizing a Commercial MNOS EEPROM for Space

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  1. Observations in Characterizing a Commercial MNOS EEPROM for Space E. E. King, R. C. Lacoe, G. Eng, and M. S. Leung The Aerospace Corporation El Segundo, CA (310) 336-7898, everett.e.king@aero.org 2004 MAPLD International Conference Ronald Reagan Building and International Trade CenterWashington, D.C. September 8-10, 2004 1

  2. Hitachi HN58C1001 Specification • 128k x 8-bit (1 Mbit) Electrically Erasable and Programmable Non-Volatile Memory • Single 5 V Power Supply (-10V programming voltage generated on chip) • Access Time 150 ns • Automatic Byte or Page (128 bytes) Write • Write Time <10 ms • 104 Erase/Write cycles • 10 year Data Retention 2

  3. Gate 28 nm Si3N4 N+ Source N+ Drain 1.6nm SiO2 P well N substrate MNOS Memory Transistor Operation • Presence or absence of charge trapped in the silicon nitride layer results in a change in Vth between two states defined as a ‘1’ and ‘0’ • Electrons are injected (write a ‘1’) by setting Vg = 5 V with -10 V applied to the well • A ‘1’ is erased (write a ‘0’) by applying 5 V to the well and setting Vg to -10 V, which injects holes • The transistor state is interrogated by detecting channel current for a Vg = 0 V • Data loss is generally due to thermal emission of the trapped charge in the silicon nitride (Ea = 1.1 eV) 3

  4. Typical Space Application • Memory written at beginning of mission • No power applied until the memory is needed to re-initialize the system • No memory rewrite planned during the mission • Memory speed is not critical • Maximum temperature is 70 C • Data must be retained for 15 years 4

  5. Our Test Objectives • Determine data retention lifetime • Stress parts at high temperature to accelerate data loss • Stress at two temperatures to determine the activation energy for the data loss process • Use data to predict data retention lifetime at 70 C • Characterize effect of TID on data retention • Develop qualification test to screen potential early failures out of the production part population • Determine worst-case test parameters • Develop worst-case test pattern 5

  6. Accelerated Aging Test Plan • Pre-condition parts • Write checkerboard and inverse checkerboard 220 times • Soak at 150 C for at least 48 hours • Age at 175 and 200 C - all leads grounded • Epoxy package material verified to be OK to >250 C • Half population written with checkerboard/half with inverse checkerboard • Parts tested at short intervals to catch early/intermittent failures (every 4 hours @ 200 C, 22 hours @ 175 C) • Determine impact of TID on aging • Irradiate parts to 78 krad in 26 krad steps (Co-60) • Repeat aging test post-radiation to assess affect of TID 6

  7. 40000 Control-Q2 553 hours 30000 951 hours 1036 hours No. of Data Byte Errors 1305 hours 20000 Rewritten 10000 0 70 75 80 85 90 95 100 CE Access Time (ns) Aging-Induced Push-Out of Read Access Time • Thermal stress produces a push-out of the read access time • The access time returns to its initial distribution after rewrite • Push-out extrapolated to 150 ns to estimate time-to-failure • Aging data at 175 and 200 C used to determine activation energy Part Thermally Stressed at 200 C 7

  8. Data Retention Lifetime • Assume that access time push-out is caused by charge leakage off the memory transistor • Push-out also might be influenced by the initial charge stored on the transistor and variations in sense amps • Error distribution vs. access time at 226 hours @ 200 C is similar to that at 1305 hours @ 175 C • Corresponds to an activation energy of 1.2 eV • Estimated time-to-failure (150 ns) at 70 C is a few hundred years • Worst-case activation energy for charge detrapping in the MNOS structure found in the literature is 0.35 eV • Estimated time for access time to reach 150 ns at 70 C based on this activation energy and our access-time push-out data is about 50 years 8

  9. Results of TID Tests • No significant degradation in performance found after 78 krad(Si) irradiation (unbiased) • Aging experiments after TID at 175 and 200 C showed the same access time push-out as had been measured in the initial aging experiments to within about 2% • Caution: The on-chip high voltage bias generator fails at 10-to-20 krad when irradiated under normal operating voltages 9

  10. OE OE CE CE I/O1 I/O1 I/O2 I/O2 Normal Waveforms Output oscillations Signature of Intermittent Readout Failure • Intermittent failure observed during aging due to oscillations on data outputs • Not clear that increasing readout access time will solve problem • Oscillations worse as Vdd is decreased • Oscillations disappear as temperature increased to 38C • Oscillation occurs long before there is a data retention problem due to aging • Oscillations spontaneously disappear in minutes to hours 0 1 10

  11. Vdd = 5.0V tce = 150 ns 40 No. of Bit Errors 30 20 10 0 20 40 60 80 Temperature (C) 0 Parametric Testing -- Effect of Ambient Temperature • Number of errors decrease as the ambient temperature is increased • Recommend testing at below room temperature to increase probability of detecting a ‘weak’ part 11

  12. Test Pattern Sensitivity • A bit failure was estimated to be 26,000 times more likely to be a ‘0’ than a ‘1’ • The worst-case pattern resulting in an error was reading a byte with all ‘0’s after reading a byte with all ‘1’s (70% of failed patterns) Data Pattern WrittenData Read Example 11111111 11111111 00000000 00111111 Error • Percentage of failed patterns decreased as the numbers of ‘1’s in the prior byte decreased 12

  13. Test Pattern Developed to Screen out Weak Parts • Pattern heavily populated with ‘0’s (over 98%) to increase probability of finding an early failure • Short sequence of patterns inserted periodically in the address space to detect pattern sensitive failures • Unique data byte inserted when each address bit first went high to ensure that each address bit toggled • New pattern estimated to be 300 times more likely to detect an error than a checkerboard pattern 13

  14. Conclusions • Data Retention Lifetime found suitable for space • Activation energy determined to be about 1.2 eV, consistent with manufacturers value • Worst-case data retention time estimated to be about 50 years • Found no TID problem up to 78k rad(Si) for unbiased irradiation • Identified a small probability for early failure due to data output oscillation • Consider operating part at Vdd>5V to eliminate oscillations • Oscillations also eliminated when operated somewhat above room temperature • Unclear that extending the readout access time can ensure correct data readout 14

  15. Conclusions (cont.) • Qualification test developed to increase probability of identifying ‘weak’ parts • Include tests conducted under worst-case parametric conditions for intermittent failure • Low Vdd • Low Temperature • Use special test patterns • High percentage of ‘0’s • Data patterns that include transitions from words with high number of ‘1’s to words containing high number of ‘0’s for every sense amplifier • Recommend eliminating any part exhibiting behavior that is inconsistent with the general population 15

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