Campaign
Thermal Cycling Campaign — Avionics Module
Repeated hot/cold cycling on avionics module with dwell monitoring at qualification temperature extremes.
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
- Thermal Cycling
- Hardware
- Avionics Module AM-07
- Configuration Revision
- Revision C
- Test Date
- 2026-07-22
- Status
- Review Required
- Evidence Completeness
- 83%
Artifact Summary
- ✓ Test DataPresent
- ⚠ Test ProcedureIncomplete
- ✓ Acceptance LimitsPresent
- ✓ Configuration InformationPresent
- ⚠ Calibration RecordsIncomplete
- ✓ Deviation RecordsPresent
Campaign Timeline
Step 1
Pre-Test Inspection
Step 2
Cycle 1 — Cold Dwell
Step 3
Cycle 2 — Hot Dwell
Step 4
Cycle 3 — Cold Dwell
Step 5
Cycle 4 — Hot Dwell
Step 6
Functional Check
Step 7
Post-Test Inspection