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Evidence for Drag Coefficient Modeling Errors near and Above the Oxygen-to-Helium Transition
Journal of Spacecraft and Rockets ( IF 1.3 ) Pub Date : 2020-11-01 , DOI: 10.2514/1.a34740
Valerie Bernstein 1 , Marcin Pilinski 1 , Delores Knipp 1
Affiliation  

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 atmospheric m...

中文翻译:

氧-氦转变附近和上方阻力系数建模误差的证据

模拟大气阻力的能力对于 1000 公里高度以下的精确卫星轨道预测至关重要。大气阻力的不确定性主要来自对大气m...
更新日期:2020-11-01
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