Sounding the atmospheric density at the altitude of LARES and AJISAI during solar cycle 24

Pardini C., Anselmo L., Lucchesi D., Peron R., Bassan M., Magnafico C., Pucacco G., Visco M.

Thermospheric Density Models  Neutral Drag  LARES  Ajisai  Aerospace Engineering  Space and Planetary Science  Solar Cycle 24 

During Solar Cycle 24, the passive spherical satellites LARES and Ajisai, placed in nearly circular orbits with mean geodetic altitudes between 1450 and 1500 km, were used as powerful tools to probe the neutral atmosphere density and the performances of six thermospheric models in orbital regimes for which the role of dominant atomic species is contended by hydrogen and helium, and accurate satellite measurements are scarce. The starting point of the analysis was the accurate determination of the secular semi-major axis decay rate and the corresponding neutral drag acceleration in a satellite centered orbital system. Then, for each satellite, thermospheric model and solar activity level, the drag coefficients capable of reproducing the orbital decay observed were found. These coefficients were finally compared with the physical drag coefficients computed for both satellites in order to assess the biases affecting the thermospheric density models. None of them could be considered unconditionally the best; the specific outcome depending on solar activity and the regions of the atmosphere crossed by the satellites. During solar maximum conditions, an additional density bias linked to the satellite orbit inclination was detected.

Source: Transactions of the Japan Society for Aeronautical and Space Sciences 64 (2021): 125–135. doi:10.2322/tjsass.64.125

Publisher: Japan Society for Aeronautical and Space Sciences., Tokyo , Giappone

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