Research Article
ACP-Based Space Systems: Design, Development, and Operation
Table 1
The overall mission parameters of Q-Sat.
| Parameter | Value |
| Structure | Spherical structure | Area-to-mass ratio | 0.001 m2/kg | Orbital altitude | 500 km | Inclination | 97.5° | Atmospheric density detection precision | 10-13 kg/m3 | Gravity recovery precision | More than 30 orders | Orbit determination precision | Better than 10 cm | Average power | 27.6 W |
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