SI-13 - Predictable Failure Prevention

a. Determine mean time to failure (MTTF) for the following system components in specific environments of operation: [Assignment: organization-defined system components]; and b. Provide substitute system components and a means to exchange active and standby components in accordance with the following criteria: [Assignment: organization-defined MTTF substitution criteria].


ID: SI-13
Enhancements:  1 | 3 | 4 | 5

Space Segment Guidance

Predictable failure prevention demands critical security components—like key management modules, encryption accelerators, or secure boot loaders—are built with reliability on par with essential bus systems (e.g., attitude control). In practice, mission planners might include redundant cryptographic chips or maintain "golden" backups of cryptographic credentials, ready to be loaded if the primary is corrupted. When a security element does fail, the satellite can automatically switch to a standby unit, logging the event in telemetry for ground review. Not every subsystem can be fully duplicated, given SWaP constraints, so programs often prioritize the components whose compromise would yield the most significant mission impact. By designing for graceful substitution and timely fault alerts, spacecraft operators ensure that even if a security mechanism degrades under cosmic ray bombardment or thermal stress, they can recover with minimal disruption to mission objectives.