ANALISIS PERILAKU HAMBATAN ATMOSFER DARI MODEL ATMOSFER DAN DATA SATELIT

Abstract

Atmospheric drag's behaviour can be shown by atmospheric drag's parameter B*. By assumming that ballistic koeffisien for each satellite is constant, according to atmospheric drag's model SGP-4, B* depends only on atmospheric density. For each altitudes, B*, according to satellite data and atmospheric models, has a different behaviour. B*'s behaviour will resemble the atmospheric density behaviour with the increase of altitudes.