An integrated tailoring model for thermal cycling tests of spacecraft electronics

Xin Yan Ji; Yun Ze Li; Jing Wang; Xiao Ning Yang; Yan Qiang Bi; Zhi Song Cao; Xi Yuan Li; Guo Qing Liu

doi:10.1109/TAES.2016.150525

An integrated tailoring model for thermal cycling tests of spacecraft electronics

Xin Yan Ji
, Yun Ze Li^*
, Jing Wang
, Xiao Ning Yang
, Yan Qiang Bi
, Zhi Song Cao
, Xi Yuan Li
, Guo Qing Liu

^*Corresponding author for this work

School of Aeronautic Science and Engineering

Beihang University
China Aerospace Science and Technology Corporation

Research output: Contribution to journal › Article › peer-review

3 Scopus citations

Abstract

Thermal tests of electronic units are critically important for the reliability validation and performance demonstration of spacecraft hardware. A tailoring equation like that provided by MIL-STD-1540s is necessary for the testing condition planning of these thermal tests, however, the tailoring equation provided by MIL-STD-1540s is mainly based on the fatigue data of solders. In this paper, a new test condition tailoring equation is proposed by introducing an integrated evaluating method for the fatigue acceleration exponent. The different thermo-mechanical fatigue mechanisms and different subsystem characteristics have been considered and discussed in the deducing of this new equation. The test precipitation efficiency (PE) of the new tailoring law has been analyzed and compared with that from the MIL-STD-1540 tailoring equations. The results are encouraging and reasonable.

Original language	English
Article number	7855576
Pages (from-to)	2685-2696
Number of pages	12
Journal	IEEE Transactions on Aerospace and Electronic Systems
Volume	52
Issue number	6
DOIs	https://doi.org/10.1109/TAES.2016.150525
State	Published - Dec 2016

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10.1109/TAES.2016.150525

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title = "An integrated tailoring model for thermal cycling tests of spacecraft electronics",

abstract = "Thermal tests of electronic units are critically important for the reliability validation and performance demonstration of spacecraft hardware. A tailoring equation like that provided by MIL-STD-1540s is necessary for the testing condition planning of these thermal tests, however, the tailoring equation provided by MIL-STD-1540s is mainly based on the fatigue data of solders. In this paper, a new test condition tailoring equation is proposed by introducing an integrated evaluating method for the fatigue acceleration exponent. The different thermo-mechanical fatigue mechanisms and different subsystem characteristics have been considered and discussed in the deducing of this new equation. The test precipitation efficiency (PE) of the new tailoring law has been analyzed and compared with that from the MIL-STD-1540 tailoring equations. The results are encouraging and reasonable.",

author = "Ji, \{Xin Yan\} and Li, \{Yun Ze\} and Jing Wang and Yang, \{Xiao Ning\} and Bi, \{Yan Qiang\} and Cao, \{Zhi Song\} and Li, \{Xi Yuan\} and Liu, \{Guo Qing\}",

note = "Publisher Copyright: {\textcopyright} 1965-2011 IEEE.",

year = "2016",

month = dec,

doi = "10.1109/TAES.2016.150525",

language = "英语",

volume = "52",

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issn = "0018-9251",

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TY - JOUR

T1 - An integrated tailoring model for thermal cycling tests of spacecraft electronics

AU - Ji, Xin Yan

AU - Li, Yun Ze

AU - Wang, Jing

AU - Yang, Xiao Ning

AU - Bi, Yan Qiang

AU - Cao, Zhi Song

AU - Li, Xi Yuan

AU - Liu, Guo Qing

PY - 2016/12

Y1 - 2016/12

N2 - Thermal tests of electronic units are critically important for the reliability validation and performance demonstration of spacecraft hardware. A tailoring equation like that provided by MIL-STD-1540s is necessary for the testing condition planning of these thermal tests, however, the tailoring equation provided by MIL-STD-1540s is mainly based on the fatigue data of solders. In this paper, a new test condition tailoring equation is proposed by introducing an integrated evaluating method for the fatigue acceleration exponent. The different thermo-mechanical fatigue mechanisms and different subsystem characteristics have been considered and discussed in the deducing of this new equation. The test precipitation efficiency (PE) of the new tailoring law has been analyzed and compared with that from the MIL-STD-1540 tailoring equations. The results are encouraging and reasonable.

AB - Thermal tests of electronic units are critically important for the reliability validation and performance demonstration of spacecraft hardware. A tailoring equation like that provided by MIL-STD-1540s is necessary for the testing condition planning of these thermal tests, however, the tailoring equation provided by MIL-STD-1540s is mainly based on the fatigue data of solders. In this paper, a new test condition tailoring equation is proposed by introducing an integrated evaluating method for the fatigue acceleration exponent. The different thermo-mechanical fatigue mechanisms and different subsystem characteristics have been considered and discussed in the deducing of this new equation. The test precipitation efficiency (PE) of the new tailoring law has been analyzed and compared with that from the MIL-STD-1540 tailoring equations. The results are encouraging and reasonable.

UR - https://www.scopus.com/pages/publications/85013498433

U2 - 10.1109/TAES.2016.150525

DO - 10.1109/TAES.2016.150525

M3 - 文章

AN - SCOPUS:85013498433

SN - 0018-9251

VL - 52

SP - 2685

EP - 2696

JO - IEEE Transactions on Aerospace and Electronic Systems

JF - IEEE Transactions on Aerospace and Electronic Systems

IS - 6

M1 - 7855576

ER -

An integrated tailoring model for thermal cycling tests of spacecraft electronics

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