INSPIRESAT-4/ARCADE : a VLEO mission for atmospheric temperature measurements and ionospheric plasma characterization
Most nano-satellite and small satellite missions are designed for 400 km or higher altitudes. This is because small satellites, with mass, volume and power constraints, have limited propulsion capabilities to counteract the high aerodynamic drag in lower altitudes. Thus little or no science data...
| Main Authors: | , , |
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| Format: | Conference Paper |
| Language: | English |
| Published: |
2021
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| Subjects: | |
| Online Access: | https://digitalcommons.usu.edu/smallsat/2019/all2019/140/ https://hdl.handle.net/10356/148434 |