Exercise
https://texercises.raemilab.ch/exercise/neptun-flieg/
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The following quantities appear in the problem: Masse \(m\) / Radius \(r\) / Umlaufzeit \(T\) /
The following formulas must be used to solve the exercise: \(\frac{T^2}{r^3} = \frac{4\pi^2}{GM} \quad \)
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Exercise:
Neptun hat eine mittlere Entfernung von r_N .^m oder AE. Wie lange dauert ein Umlauf um die Sonne?

Solution:
Es gilt: fracT_N^T_E^ fracr_N^r_E^ Rightarrow T_N sqrtfracr_N^r_E^ T_E^ approx jahr.
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Exercise:
Neptun hat eine mittlere Entfernung von r_N .^m oder AE. Wie lange dauert ein Umlauf um die Sonne?

Solution:
Es gilt: fracT_N^T_E^ fracr_N^r_E^ Rightarrow T_N sqrtfracr_N^r_E^ T_E^ approx jahr.
Contained in these collections
  1. Kepler 3 by TeXercises
    3 | 8
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Tags
himmelsmechanik, keplersche gesetze, mechanik
Difficulty
(1, default)
Points
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Language
GER (Deutsch)
Type
Calculative / Quantity
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