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Notes on the Reliability of The HST Gyros
File Name: 25093003.pdf | Date Submitted: 01/28/02
 

File Size:
2372KB
Document Author
Henning Leidecker - henning.w.leidecker@nasa.gov
Goddard Space Flight Center
Phone: 301 286-9180 | FAX: 301 286-1695
[Additional User Information]

Download "Notes on the Reliability of The HST Gyros" (2372KB) Now.
 
Description:
The gyro failures
 
Abstract:

The most important failure mode of the HST gyros is flex lead rupture,caused by corrosion.This mechanism is characterized by a failure rate that is initially vanishingly low,and rises to large values only after a threshold time (determined mainly by the corrosion rate and not the initial strength of the flex leads) is passed.The threshhold time is a random variable,and so the failure time is also a random variable.The observed five times-to-fracture and the eleven observed operating times with no fracture,among the sixteen gyros to operate so far,are well fit using a Weibull Probability Law with time- scale n = 5.89 yr.and shape-parameter B =4.82: the correlation coefficient is r =0.989. This fit excludes the previously used Exponential Probability Law with better than 95% confidence.The total Probability Law for the lifetime of an HST gyro is the product of the Weibull Law for corrosion-induced rupture,with an Exponential Probability Law describing the other failure modes (electronic failure and lube patch failure)and an estimate of the latter;s mean-time-to-failure is roughly 28 yr.

 

 
Related Project(s):
EPAC (Electronic Packaging)
EPAR (Electronic Parts)
 
Related Area(s) of Emphasis:
Advanced Sensors/Detectors
Advanced Interconnect Reliability

 
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