Boards
| Board | Description |
|---|---|
| MB | Mission board |
| RAB | Gyro, gyro MCU and camera |
| ANT | Antenna board |
| BPB | Backplane, current sensors |
| OBC | Micro Orbiter 1 derived board |
| FAB | BIRDS-5 derived board |
| COM | Communication board |
| Arduino R4 compatible board | Gyro MCU |
| +Z panel | CIGS solar cells |
| −Z panel | Status LEDs, 2 circuits, 4 LEDs |
| −X, +Y, −Y panels | Common design with YOMOGI |
| Main structure | Common design with YOMOGI |
Antenna
| Test | Result |
|---|---|
| Deployment rate, 20 times | 100% |
| Deployment time | Within 20 s |
| Hot deployment | 24 s |
| Cold deployment, −35 ℃ | Pass |
| Deployment force | 0.56 kgf, creep test load 1.96 kgf |
| Wire strength | Creep, strength and proof tests passed |
Inspections
| Test | Result |
|---|---|
| Fit Check | Pass |
| Interface Verification | Pass |
| Sharp Edge Inspection | Pass |
| Inhibit | Diode reverse current within 600 µA, DCDC output 4.21 V or less |
| SAP | IV curve change within 10% before and after TVT |