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Evaluation of Radiation Effects in Flash Memories Tetsuo Miyahira ...

Evaluation of Radiation Effects in Flash Memories Tetsuo Miyahira ...

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irradiation to 143 seconds at 12 krads for the worst <strong>of</strong> the<br />

six test devices.<br />

Supply current (Idd) degradation<br />

In the plot entitled “Supply Current (Idd)” shows that Idd<br />

for the Samsung device began to rise rapidly at about 8<br />

krads and the device failed functionally at about ~10<br />

krads. Idd for the Intel device began to rise rapidly at<br />

about 20 krads and the device failed functionally at<br />

~24 krads.<br />

V. SEU RESULTS<br />

SEU Tests<br />

Unpowered mode. The purpose <strong>of</strong> this test was to<br />

determ<strong>in</strong>e if the float<strong>in</strong>g gate would upset with heavy<br />

ions. <strong>Flash</strong> memories use an embedded microcontroller<br />

to improve erase/write times. The device was left<br />

unpowered, dur<strong>in</strong>g irradiation, to prevent upsets <strong>in</strong> the<br />

microcontroller, which <strong>in</strong> turn could cause an upsets <strong>in</strong><br />

the memory cells. The memory was loaded with a known<br />

pattern prior to the test and left unpowered while be<strong>in</strong>g<br />

irradiated with heavy ions. After the irradiation, the<br />

device was powered and tested to see if there were any<br />

changes to the pattern. No cell upset occurred when<br />

tested <strong>in</strong> this mode even up to an effective LET <strong>of</strong> 120<br />

MeV-cm 2 /mg.<br />

Static mode. For this mode, the flash memory was<br />

powered but there was no active address<strong>in</strong>g tak<strong>in</strong>g place<br />

dur<strong>in</strong>g irradiation. Most <strong>of</strong> the test<strong>in</strong>g was done us<strong>in</strong>g<br />

this mode. Before the irradiation, the device was loaded<br />

with a known pattern and at the completion <strong>of</strong> the<br />

irradiation, the device was tested to see if the memory<br />

content had changed. When test<strong>in</strong>g <strong>in</strong> this mode,<br />

functional <strong>in</strong>terrupts (SEFIs) would occur that <strong>in</strong> most<br />

cases required power cycl<strong>in</strong>g (turn<strong>in</strong>g Vdd <strong>of</strong>f and then on<br />

aga<strong>in</strong>) to clear the error condition. We were able to<br />

identify seven error modes (lockup conditions). Besides<br />

the seven error modes, three Intel devices had<br />

catastrophic high current condition that occurred dur<strong>in</strong>g<br />

functionality test after the irradiation was completed. We<br />

did not experience this catastrophic high current<br />

condition with the Samsung memories.<br />

We had no visibility <strong>of</strong> functionality dur<strong>in</strong>g irradiation,<br />

because we were not address<strong>in</strong>g the test device when<br />

tested <strong>in</strong> the static mode. Each irradiation run therefore<br />

became a pass or fail test. In order to determ<strong>in</strong>e a cross<br />

section, we selected fluence so that some <strong>of</strong> the runs<br />

resulted <strong>in</strong> a SEFI and some did not. Cross section was<br />

determ<strong>in</strong>ed by add<strong>in</strong>g the number <strong>of</strong> SEFIs then divid<strong>in</strong>g<br />

by the total fluence (passes as well as fails). The plot <strong>of</strong><br />

3<br />

the cross section as a function <strong>of</strong> LET for the Intel<br />

28F016SV is shown on the graph entitled “Cross Section<br />

for Complex Functional Upset Modes.” The error bars<br />

are large because we did not know at what po<strong>in</strong>t dur<strong>in</strong>g<br />

the irradiation the SEFI occurred or if more than one<br />

SEFI occurred dur<strong>in</strong>g that run.<br />

Read mode and erase/write mode. Most <strong>of</strong> the time<br />

was spent test<strong>in</strong>g <strong>in</strong> the static mode. The results from<br />

tests <strong>in</strong> read and erase/write modes were too limited to<br />

<strong>in</strong>clude <strong>in</strong> this paper. We will address these modes<br />

further <strong>in</strong> future tests.<br />

Isolat<strong>in</strong>g the memory array<br />

We used a copper shield to mask <strong>of</strong>f the microcontroller.<br />

The diagram entitled “Chip Micrograph” shows the area<br />

that was masked from the heavy ions. This was done to<br />

see if memory upsets would still occur. We got mixed<br />

results from this test, possibly because the sens<strong>in</strong>g and<br />

high voltage circuitry was <strong>in</strong>terspersed with the memory<br />

array, and could not be masked. With the Intel<br />

28F016SA memories, we observed no errors. The<br />

28F016SV (smart voltage) devices, however, did appear<br />

to exhibit memory errors at very high LET. However,<br />

the cross section was very low, and it is likely that the<br />

apparent memory errors are caused by the response <strong>of</strong> the<br />

more complex SV microcontroller. Accord<strong>in</strong>g to the<br />

manufacturer, the SV and SA memory cell technologies<br />

are identical and should have behaved similarly.<br />

VI. PLAN FOR FOLLOW ON TESTS<br />

X2000 Project<br />

X2000 Project is driv<strong>in</strong>g the flash memory survey. There<br />

are currently five missions proposed for X2000 project<br />

(Europa, Pluto, Solar Probe, Champollion, and a Mars<br />

mission). The <strong>Radiation</strong> <strong>Effects</strong> Group at JPL is<br />

primarily concerned with the Europa spacecraft because<br />

<strong>of</strong> its severe radiation environment. The Europa<br />

spacecraft is expected to be exposed to mostly electron<br />

dose <strong>of</strong> about four megarad(Si), beh<strong>in</strong>d 100 mils <strong>of</strong><br />

alum<strong>in</strong>um. Design trade studies <strong>in</strong>dicate that it is<br />

possible to shield to about 40 krad(Si) <strong>in</strong> order to ga<strong>in</strong> the<br />

advantages <strong>of</strong> us<strong>in</strong>g commercial flash and /or DRAMS as<br />

opposed to us<strong>in</strong>g an all radiation hardened SRAM. If we<br />

are able to f<strong>in</strong>d a suitable flash memory, the X2000<br />

modular architecture needs at least one giga-bit and<br />

would like eight giga-bits <strong>of</strong> flash memory for each<br />

spacecraft. The follow-on flash memory evaluation will<br />

be done <strong>in</strong> three steps, as described below.<br />

S<strong>in</strong>gle Event Latchup (SEL) test and cursory S<strong>in</strong>gle<br />

Event Upset (SEU) tests

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