Table 4.
Size, power, data rate and mass of subsystems. Values given with 20% margin (10% for fuel and avionics).
| Size (cm) | Power (W) | Data (bps) | Mass (kg) | ||
|---|---|---|---|---|---|
| Bus | Structure | 110 × 110 × 100 | N/A | N/A | 325 |
| Avionics | 35 × 25 × 50 | 40 (61 peak) | N/A | 12 | |
| Communication | 35 × 25 × 50 | 15 (50 peak) | N/A | 10 | |
| Bus Total | N/A | 55 (111 peak) | N/A | 347 | |
| Payload | INMS | 10 × 10 × 10 | 3 | 2048 | 3.6 |
| IVM | 25 × 12 × 9 | 3 | 2000 | 2.6 | |
| m-NLP | 10 × 7.5 × 5 | 3.5 | 1900 | 0.3 | |
| Thermistors | 3.3 × 0.066 × 0.066 | 0.01 | 96 | 0.036 | |
| CITRIS | 40 × 31 × 12 | 12.3 | 15,000 | 5.4 | |
| IGOR | 21.8 × 24 × 14.4 | 22 | 20,000 | 6.96 | |
| ISA | 3.1 × 1.7 × 1.3 | 12.1 | 9600 | 9.78 | |
| FGM | 10 × 10 × 10 | 0.8 | 400 | 1.8 | |
| Boom | 100 | N/A | N/A | 3 | |
| Payload total | N/A | 57 | 50 k | 35 | |
| Total dry mass | 382 | ||||
| Fuel | 165 | ||||
| Total (wet mass) | N/A | 112 (168 peak) | 50 k | 547 |
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