• Engineering
  • Published 2016

Reliable design of micro-satellite systems using combined physics of failure reliability estimation models

@inproceedings{Hussmann2016ReliableDO,
  title={Reliable design of micro-satellite systems using combined physics of failure reliability estimation models},
  author={Cass Adam Hussmann},
  year={2016}
}
Up until 2015 the rate at which cube satellite missions achieved full mission success was only 44.1% for any organizations first mission (academic or corporate), the success rate increases to only 62% for cube satellites launched as a second mission. This thesis suggests that there are two main sources for the high failure rate: improper verification, and the common use of COTS components and their reliability in a space environment. The thesis provides a means of increasing mission assurance… CONTINUE READING

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