REG NASA-LLIS-0275--1993 Lessons Learned Stressed or Damaged Solder Joints on Flight Hardware Due to Thermal Cycling.pdf
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1、Lessons Learned Entry: 0275Lesson Info:a71 Lesson Number: 0275a71 Lesson Date: 1993-07-09a71 Submitting Organization: JPLa71 Submitted by: T. Borden / B. WagonerSubject: Stressed or Damaged Solder Joints on Flight Hardware Due to Thermal Cycling Abstract: Over the years, numerous incidents of failed
2、 solder joints have occurred to electronic equipment at JPL and contractor facilities. The problem was traced to thermal cycling of conformal coatings.The lesson recommendations pertain to prediction of the thermal cycling environment, application of conformal coatings, packaging design reviews, and
3、 packaging design and fabrication processes, procedures, and documentation. Description of Driving Event: During recent years numerous incidents of failed solder joints in electronic equipment have been identified in hardware fabricated both at JPL and JPL Contractor facilities. Examples include:1.
4、GALILEO, PFR #52012, Command Data Subsystem: Intermittent failure in solder joints at flat pack lead attachment to the printed wiring board.2. ASTROS Star Tracker, PFR #33998, Electronic Assembly failure: Solder connection open at a Dual Inline Package Integrated Circuit (DIP IC) lead to the printed
5、 wiring board.3. MAGELLAN, PFR #55263, Data Formatter, Electronic Assembly failure: Solder connection open at a DIP IC lead to printed wiring board.4. WF/PC-1 PFR #53914 Microprocessor failure: Solder connection open at a DIP IC lead to printed wiring board.5. ACRIM II, PFR #44478: Electronic Module
6、 solder joints were observed to have stressing/cracking at the DIP IC lead to printed wiring board interconnect.6. MLS, PFR #43374: Solder joint on input bias wire had stress cracks.Investigation of the above items reveal a common element of cause. Conformal coating (polymeric Provided by IHSNot for
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