Campaign
Vibration Qualification — Flight Computer
Sine sweep and random vibration qualification on flight computer with triaxial accelerometer monitoring.
Test type: VibrationHardware: Flight Computer FC-3Configuration: Revision AReview RequiredEvidence completeness: 75%
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.
Campaign Summary
- Test Type
- Vibration
- Hardware
- Flight Computer FC-3
- Configuration Revision
- Revision A
- Test Date
- 2026-06-03
- Status
- Review Required
- Evidence Completeness
- 75%
Artifact Summary
- ✓ Test DataPresent
- ✓ Test ProcedurePresent
- ✓ Acceptance LimitsPresent
- ⚠ Configuration InformationIncomplete
- ✓ Calibration RecordsPresent
- ✗ Deviation RecordsMissing
Campaign Timeline
Step 1
Pre-Test Inspection
Step 2
Low-Level Sine Sweep
Step 3
Qualification Random Vibration
Step 4
Post-Vibe Functional Test
Step 5
Post-Test Inspection