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Single-Event Latchup Testing of the Micrel MIC4424 Dual Power MOSFET DriverWe conducted 47 exposures of four different MIC4424 devices and did not observe any SEL or high-current events. This included worst-case conditions with a LET of 81 MeV-sq cm/mg, applied voltage of 18.5 V, a case temperature greater than 120 C, and a final fluence of 1x10(exp 7)/sq cm. We also monitored both the outputs for the presence of SETs. While the period of the 1 MHz square wave was slightly altered in some cases, no pulses were added or deleted. 1. Purpose: The purpose of this testing is to characterize the BiCMOS/DMOS Micrel MIC4424 dual, non-inverting MOSFET driver for single-event latchup (SEL) susceptibility. These data will be used for flight lot evaluation purposes. 2. Devices Tested: The MIC4423/4424/4425 family are highly reliable BiCMOS/DMOS buffer/driver MOSFET drivers. They are higher output current versions of the MIC4426/4427/4428. They can survive up to 5V of noise spiking, of either polarity, on the ground pin. They can accept, without either damage or logic upset, up to half an amp of reverse current (either polarity) forced back into their outputs. Primarily intended for driving power MOSFETs, the MIC4423/4424/4425 drivers are suitable for driving other loads (capacitive, resistive, or inductive) which require low-impedance, high peak currents, and fast switching times. Heavily loaded clock lines, coaxial cables, or piezoelectric transducers are some examples. The only known limitation on loading is that total power dissipated in the driver must be kept within the maximum power dissipation limits of the package. Five (5) parts were provided for SEL testing. We prepared four parts for irradiation and reserved one piece as an un-irradiated control. More information about the devices can be found in Table 1. The parts were prepared for testing by removing the lid from the CDIP package to expose the target die. The parts were then soldered to small copper circuit adapter boards for easy handling. These parts are fabricated in a bulk BiCMOS/DMOS technology. Since we do not know the number of overlayers used in the fabrication processes, linear energy transfer calculations are determined based on the top-surface incident ion species and kinetic energy.
Document ID
20160014608
Acquisition Source
Goddard Space Flight Center
Document Type
Other
Authors
Pellish, J. A.
(NASA Goddard Space Flight Center Greenbelt, MD United States)
Boutte, A.
(NASA Goddard Space Flight Center Greenbelt, MD United States)
Kim, H.
(ASRC Federal Space and Defense Greenbelt, MD, United States)
Phan, A.
(ASRC Federal Space and Defense Greenbelt, MD, United States)
Topper, A.
(ASRC Federal Space and Defense Greenbelt, MD, United States)
Date Acquired
December 14, 2016
Publication Date
December 10, 2016
Subject Category
Electronics And Electrical Engineering
Report/Patent Number
GSFC-E-DAA-TN36552
Report Number: GSFC-E-DAA-TN36552
Funding Number(s)
CONTRACT_GRANT: NNG13CR48C
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
Power MOSFET
Single-Event Latchup (SEL)
Test Report
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