Anomaly Review
Open a campaign to inspect the evidence chain for each finding.
| Severity | Anomaly | Campaign |
|---|---|---|
| Critical | Temperature Sensor A exceeded the qualification upper limit. | TVAC Qualification Campaign — Satellite Payload A |
| High | Pressure data missing for a significant period. | TVAC Qualification Campaign — Satellite Payload A |
| High | Temperature Sensor A and Temperature Sensor B diverged beyond the redundant-sensor threshold. | TVAC Qualification Campaign — Satellite Payload A |
| Critical | Module Temperature A exceeded the qualification upper limit. | Thermal Cycling Campaign — Avionics Module |
| Medium | Sudden Module Temperature A change. | Thermal Cycling Campaign — Avionics Module |
| Medium | Sudden Module Temperature A change. | Thermal Cycling Campaign — Avionics Module |
| Medium | Sudden Module Temperature A change. | Thermal Cycling Campaign — Avionics Module |
| Medium | Sudden Module Temperature A change. | Thermal Cycling Campaign — Avionics Module |
| Medium | Sudden Module Temperature A change. | Thermal Cycling Campaign — Avionics Module |
| Medium | Sudden Module Temperature A change. | Thermal Cycling Campaign — Avionics Module |
| Medium | Sudden Module Temperature A change. | Thermal Cycling Campaign — Avionics Module |
| Medium | Sudden Module Temperature A change. | Thermal Cycling Campaign — Avionics Module |
| Medium | Sudden Module Temperature A change. | Thermal Cycling Campaign — Avionics Module |
| Medium | Sudden Module Temperature A change. | Thermal Cycling Campaign — Avionics Module |
| Medium | Sudden Module Temperature A change. | Thermal Cycling Campaign — Avionics Module |
| Medium | Sudden Module Temperature A change. | Thermal Cycling Campaign — Avionics Module |
| Medium | Sudden Module Temperature B change. | Thermal Cycling Campaign — Avionics Module |
| Medium | Sudden Module Temperature B change. | Thermal Cycling Campaign — Avionics Module |
| Medium | Sudden Module Temperature B change. | Thermal Cycling Campaign — Avionics Module |
| Medium | Sudden Module Temperature B change. | Thermal Cycling Campaign — Avionics Module |
| Medium | Sudden Module Temperature B change. | Thermal Cycling Campaign — Avionics Module |
| Medium | Sudden Module Temperature B change. | Thermal Cycling Campaign — Avionics Module |
| Medium | Sudden Module Temperature B change. | Thermal Cycling Campaign — Avionics Module |
| Medium | Sudden Module Temperature B change. | Thermal Cycling Campaign — Avionics Module |
| Medium | Sudden Module Temperature B change. | Thermal Cycling Campaign — Avionics Module |
| Medium | Sudden Module Temperature B change. | Thermal Cycling Campaign — Avionics Module |
| Medium | Sudden Module Temperature B change. | Thermal Cycling Campaign — Avionics Module |
| High | Module Temperature A and Module Temperature B diverged beyond the redundant-sensor threshold. | Thermal Cycling Campaign — Avionics Module |
| Critical | X-axis Acceleration exceeded the qualification upper limit. | Vibration Qualification — Flight Computer |
| Medium | Sudden X-axis Acceleration change. | Vibration Qualification — Flight Computer |
| Medium | Sudden X-axis Acceleration change. | Vibration Qualification — Flight Computer |
| Medium | Sudden X-axis Acceleration change. | Vibration Qualification — Flight Computer |
| Medium | Sudden X-axis Acceleration change. | Vibration Qualification — Flight Computer |
| Medium | Sudden Y-axis Acceleration change. | Vibration Qualification — Flight Computer |
| Medium | Sudden Y-axis Acceleration change. | Vibration Qualification — Flight Computer |
| High | X-axis Acceleration and Y-axis Acceleration diverged beyond the redundant-sensor threshold. | Vibration Qualification — Flight Computer |
| High | X-axis Acceleration and Y-axis Acceleration diverged beyond the redundant-sensor threshold. | Vibration Qualification — Flight Computer |
| High | X-axis Acceleration and Y-axis Acceleration diverged beyond the redundant-sensor threshold. | Vibration Qualification — Flight Computer |
| High | X-axis Acceleration and Y-axis Acceleration diverged beyond the redundant-sensor threshold. | Vibration Qualification — Flight Computer |
| High | X-axis Acceleration and Y-axis Acceleration diverged beyond the redundant-sensor threshold. | Vibration Qualification — Flight Computer |
| High | X-axis Acceleration and Y-axis Acceleration diverged beyond the redundant-sensor threshold. | Vibration Qualification — Flight Computer |