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- W2084043029 abstract "Abstract The planar motion approximation is adequate for re-entry deceleration and heating rate studies. However if the analysis is continued to lower altitudes, we can not any more assume the motion to take place in a fixed plane. In equatorial and midlatitude re-entries with CDA/m = 0.1 m2/kg the atmospheric rotation results in appreciable rotation of the orbital plane from the altitude of 60 km. With CDA/m = 0.001 m2/kg the marked rotation begins at the altitude of 30 km. These results were obtained by calculations using the method outlined in this paper to determine Ω and i as functions of altitude during re-entry. Further we define the conception of relaxed re-entry and give an algorithm to get the impact values of Ω and i. Finally we give an approximate expression for the eastward shift of the impact point due to atmospheric rotation." @default.
- W2084043029 created "2016-06-24" @default.
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- W2084043029 date "1971-10-01" @default.
- W2084043029 modified "2023-09-25" @default.
- W2084043029 title "On the rotation of the orbital plane during ballistic re-entry" @default.
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- W2084043029 doi "https://doi.org/10.1016/0032-0633(71)90178-4" @default.
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