Exercise
https://texercises.com/exercise/minimum-energy-to-place-sputnik-1-into-orbit/
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The following quantities appear in the problem: Masse \(m\) / Kraft \(F\) / Arbeit \(W\) / Geschwindigkeit \(v\) / Strecke \(s\) / Radius \(r\) / Winkelgeschwindigkeit / Kreisfrequenz \(\omega\) /
The following formulas must be used to solve the exercise: \(W = \int F(s)\,\text{d}s \quad \) \(F = G \dfrac{m_1m_2}{r^2} \quad \) \(F = m\dfrac{v^2}{r} \quad \) \(F = mr\omega^2 \quad \)
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Exercise:
The first artificial Earth satellite was the Soviet Sputnik . It had a mass of mO and reached a nearly circular orbit at an altitude of approximately hO above the Earth's surface in October . Calculate the minimum mechanical energy that the R- launch vehicle had to supply in order to place the satellite o this orbit.

Solution:
The satellite’s orbital period is determined by sscFZ &mustbe sscFG mromega^ fracGMmr^ omega sqrtfracGMr^ sqrtfracncG MR+h^ w T fracpiomega pi sqrtfracr^GM fracpiw T approx TmP ThP The energy that had to be supplied to the satellite has two components: kinetic energy and potential energy. The potential energy is: sscEpot _R^R+hfracGMmr^ mboxdr GMm leftfracR-fracR+hright Ep The kinetic energy of the satellite is: sscEkin frac mv^ frac mr^omega^ frac m R+h^ Ek So the satellite must have a total energy of: E sscEpot + sscEkin Ep + Ek E approx ES EP
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Exercise:
The first artificial Earth satellite was the Soviet Sputnik . It had a mass of mO and reached a nearly circular orbit at an altitude of approximately hO above the Earth's surface in October . Calculate the minimum mechanical energy that the R- launch vehicle had to supply in order to place the satellite o this orbit.

Solution:
The satellite’s orbital period is determined by sscFZ &mustbe sscFG mromega^ fracGMmr^ omega sqrtfracGMr^ sqrtfracncG MR+h^ w T fracpiomega pi sqrtfracr^GM fracpiw T approx TmP ThP The energy that had to be supplied to the satellite has two components: kinetic energy and potential energy. The potential energy is: sscEpot _R^R+hfracGMmr^ mboxdr GMm leftfracR-fracR+hright Ep The kinetic energy of the satellite is: sscEkin frac mv^ frac mr^omega^ frac m R+h^ Ek So the satellite must have a total energy of: E sscEpot + sscEkin Ep + Ek E approx ES EP
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Attributes & Decorations
Branches
Gravitation, Work, Energy, Power
Tags
arbeitsintegral, energie, gravitation, integralrechnung, kinetische energie, mechanik, physik, satellit, umlaufzeit, usa, zentripetalkraft
Content image
Difficulty
(3, default)
Points
4 (default)
Language
ENG (English)
Type
Calculative / Quantity
Creator uz
Decoration
File
Link