MHB How much work is required to lift a weight to orbit?

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The discussion centers on calculating the work required to lift a 100-kilogram weight to an orbit 35,786 kilometers above Earth. The initial calculations provided an incorrect estimate of approximately 5.3 billion Newton meters. The correct approach involves using the gravitational force formula and integrating to find the work done, resulting in approximately 5.311 billion joules. Participants express confusion over the calculations, particularly those without a physics background. The thread highlights the complexities involved in gravitational work calculations.
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9.5.1 work integral

How much work is done in lifting a $100$ kilogram weight from the surface of the Earth to an orbit $35,786$ kilometers above the surface of the earth?

Answer $\approx 5, 305, 028, 517$ Newton meters

$$6371=r_0$$
$$35786+r_0 = D$$
$$k=r_0^2\cdot100\approx4058964100$$
$$W=\int_{r_0}^{D} \frac{k}{{r}^{2}}\,dr \approx 540817.9092$$

Obviously didn't get the answer??
 
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karush said:
9.5.1 work integral

How much work is done in lifting a $100$ kilogram weight from the surface of the Earth to an orbit $35,786$ kilometers above the surface of the earth?

Answer $\approx 5, 305, 028, 517$ Newton meters

$$6371=r_0$$
$$35786+r_0 = D$$
$$k=r_0^2\cdot100\approx4058964100$$
$$W=\int_{r_0}^{D} \frac{k}{{r}^{2}}\,dr \approx 540817.9092$$

Obviously didn't get the answer??

Hi karush! ;)

The force of gravity is:
$$F_g = \frac{GMm}{r^2}$$
So:
$$\begin{aligned}W &= \int_{r_0}^D \frac{GMm}{r^2} \,dr = \left. -\frac{GMm}{r} \right|_{r_0}^D = GMm\left(\frac 1 {r_0} - \frac 1 D\right) \\
&= 3.986004418\cdot 10^{14} \cdot 100 \cdot \left(\frac 1 {6371\cdot 10^{3}} - \frac 1 {(35786+6371)\cdot 10^{3}}\right) \\
&= 5.311\cdot 10^{9}\text{ J}
\end{aligned}$$
 
Thanks
Don't have any physics background 😩😩😩
 
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