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Evaluation of Automotive Grade Resistors for Space FlightOver the past decade, electronic, electrical, and electromechanical (EEE) parts for space applications have undergone significant changes, largely driven by CubeSat and commercial space developers pushing the boundaries on the utilization of commercial parts in space. Global product shortages and shipping delays are still impacting space flight project deadlines. Many projects have turned to automotive grade resistors as an alternate to their MILSPEC counterparts to fulfill requirements. In addition, automotive grade resistors may offer designers a wider range of parts to consider. 

A recent NASA study recommended the use of high-volume manufactured commercial components for space applications provided these components show evidence of stringent fabrication controls and thorough reliability monitoring practices. Automotive grade components have stringent qualification requirements per the Automotive Electronic Council (AEC). However, the end user usually does not have insight into the practices the manufacturer may use to reduce/eliminate infant mortality nor for compliance to all datasheet specifications.

Screening, Life and Accelerated Life testing on a set of standard automotive-grade chip resistors is proposed to evaluate the reliability of these components. Requirements from both the AEC-Q (Automotive Electronic Council Qualification) and EEE-INST-002 (Instructions for EEE Parts Selection, Screening, Qualification, and Derating) for resistors is compared and discussed. The resistors have been tested by using a modified methodology from EEEINST-002 to evaluate their reliability for space flight projects.

The findings of this study indicate that the underlying degradation mechanisms at rated temperature and power are best represented by power law models with a fitted exponent between 0 and 1. A linear model is more conservative which compensates for potential model uncertainty given the wide range of design and materials used in automotive resistors, while still providing useful long-term resistance drift estimates. No electrical anomalies or failures were observed throughout the 1000-hour Life Tests other than small in tolerance resistance drift aging. Degradation models were utilized to quantify and extrapolate the long-term resistance drift under operating conditions for the components. The models demonstrated that some automotive-grade resistors are likely to operate 10 years at nominal usage conditions while others might fail earlier.
Document ID
20240010887
Acquisition Source
Goddard Space Flight Center
Document Type
Conference Paper
External Source(s)
Authors
Zainab Abdullahi
(Goddard Space Flight Center Greenbelt, United States)
Tristan Epp Schmidt
(Goddard Space Flight Center Greenbelt, United States)
Susana Douglas
(Goddard Space Flight Center Greenbelt, United States)
Timothy Mondy
(Goddard Space Flight Center Greenbelt, United States)
Christopher Tiu
(Goddard Space Flight Center Greenbelt, United States)
Linh Le
(Blue Origin)
Date Acquired
August 22, 2024
Subject Category
Electronics and Electrical Engineering
Meeting Information
Meeting: 5th Space Passive Component Days - SPCD 2024
Location: Noordwijk
Country: NL
Start Date: October 15, 2024
End Date: October 18, 2024
Sponsors: European Space Agency
Funding Number(s)
WBS: 817091.40.31.51.02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Technical Review
Single Expert
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