Evidence for drag coefficient modeling errors near and above the oxygen-to-helium transition

V Bernstein, M Pilinski, D Knipp - Journal of Spacecraft and Rockets, 2020 - arc.aiaa.org
The ability to model atmospheric drag is critical for precise satellite orbit prediction below
1000 km altitudes. Uncertainty in atmospheric drag comes primarily from estimates of the …
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[引用][C] Evidence for Drag Coefficient Modeling Errors near and Above the Oxygen-to-Helium Transition

V Bernstein, M Pilinski, D Knipp - Journal of Spacecraft and …, 2020 - ui.adsabs.harvard.edu
Evidence for Drag Coefficient Modeling Errors near and Above the Oxygen-to-Helium
Transition - NASA/ADS Now on home page ads icon ads Enable full ADS view NASA/ADS …
[PDF] researchgate.net

[PDF][PDF] Evidence for Drag Coefficient Modeling Errors Near and Above the Oxygen-to-Helium Transition

V Bernstein, M Pilinski, D Knipp - researchgate.net
A drag is the most uncertain perturbing force on the orbital trajectories of satellites in Low
Earth Orbit (LEO), 200-2000 km in altitude. Over 1700 satellites operate in this region [1, 2] …