Evidence Graph
Open a campaign traceability graph to inspect the evidence that supports each finding.
Demo scenario
TVAC — Satellite Payload A
Thermal Vacuum
Temperature limit violation, pressure data gap, redundant sensor divergence during hot plateau.
Thermal Cycling — Avionics Module
Thermal Cycling
Hot dwell temperature excursion above acceptance limit during cycle 4.
Vibration — Flight Computer
Vibration
X-axis acceleration spike exceeding qualification limit during random vibration segment.
Open discovery workspace for interview notes, guided demo, and design-partner intake.
Select a scenario above, then open the Traceability tab on the campaign.