Thermospheric mass density: A review

JT Emmert - Advances in Space Research, 2015 - Elsevier
The mass density of Earth's thermosphere (∼ 90–600 km altitude) is a critical parameter for
low Earth orbit prediction because of the atmospheric drag on satellites in this region. In this …

Study on the thermospheric density distribution pattern during geomagnetic activity

L Yin, L Wang, L Ge, J Tian, Z Yin, M Liu, W Zheng - Applied Sciences, 2023 - mdpi.com
The atmospheric density of the thermosphere is a fundamental parameter for spacecraft
launch and orbit control. Under magnetic storm conditions, the thermospheric atmospheric …

[HTML][HTML] Satellite drag coefficient modeling for thermosphere science and mission operations

PM Mehta, SN Paul, NH Crisp, PL Sheridan… - Advances in Space …, 2023 - Elsevier
Satellite drag modeling remains the largest source of uncertainty affecting space operations
in low Earth orbit. The uncertainty stems from inaccurate models for mass density and drag …

Thermosphere densities derived from Swarm GPS observations

J van den IJssel, E Doornbos, E Iorfida, G March… - Advances in Space …, 2020 - Elsevier
After the detection of many anomalies in the Swarm accelerometer data, an alternative
method has been developed to determine thermospheric densities for the three-satellite …

High-fidelity geometry models for improving the consistency of CHAMP, GRACE, GOCE and Swarm thermospheric density data sets

G March, EN Doornbos, P Visser - Advances in Space Research, 2019 - Elsevier
During the last two decades, accelerometers on board of the CHAMP, GRACE, GOCE and
Swarm satellites have provided high-resolution thermosphere density data to improve our …

Gas-surface interactions modelling influence on satellite aerodynamics and thermosphere mass density

G March, J Van Den Ijssel, C Siemes… - Journal of Space …, 2021 - swsc-journal.org
The satellite acceleration data from the CHAMP, GRACE, GOCE, and Swarm missions
provide detailed information on the thermosphere density over the last two decades. Recent …

Drag coefficient model using the Cercignani–Lampis–Lord gas–surface interaction model

A Walker, P Mehta, J Koller - Journal of Spacecraft and Rockets, 2014 - arc.aiaa.org
Drag coefficient calculations using the Cercignani–Lampis–Lord quasi-specular gas–
surface interaction model have been used to derive modified closed-form solutions for …

ADBSat: Methodology of a novel panel method tool for aerodynamic analysis of satellites

LA Sinpetru, NH Crisp, D Mostaza-Prieto… - Computer Physics …, 2022 - Elsevier
ADBSat is a novel software that determines the aerodynamic properties of any body in free-
molecular flow. Its main advantage is the fast approximation of the aerodynamics of …

Comparing physical drag coefficients computed using different gas–surface interaction models

PM Mehta, A Walker, CA McLaughlin… - Journal of Spacecraft and …, 2014 - arc.aiaa.org
Drag coefficient is a major source of uncertainty in calculating the aerodynamic forces on
satellites in low Earth orbit. Closed-form solutions are available for simple geometries under …

Performance characterization and kinetic analysis of atmosphere-breathing electric propulsion intake device

G Moon, M Yi, K Park, Y Kim, H Yoon, E Jun - Vacuum, 2023 - Elsevier
An atmosphere-breathing electric propulsion (ABEP) system is designed to capture and
compress the rarefied atmosphere through an intake device in very-low-Earth-orbit (VLEO) …