Question 13 Marks
The geostationary orbit of the earth is at a distance of about $36000\ km$ from the earth's surface. Find the weight of a $120\ kg $ equipment placed in a geostationary satellite. The radius of the earth is $6400\ km.$
Answer
View full question & answer→The geostationary orbit of the Earth is at a distance of about $36000\ km.$
We know that the value acceleration due to gravity above the surface of the Earth is given by $\text{g}'=\frac{\text{Gm}}{(\text{R + h})^2}.$
At h = 36000km, we have:$\text{g}'=\frac{\text{Gm}}{(36000+6400)^2}$
At the surface, we have:$\text{g}=\frac{\text{Gm}}{(6400)^2}$
$\therefore\frac{\text{g}'}{\text{g}}=\frac{6400\times6400}{42400\times42400}$
$=\frac{256}{106\times106}=0.0228$
$\Rightarrow\text{g}'=0.0227\times9.8=0.223 [$Taking $g = 9.8m/s^2$ at the surface of the earth$]$
For a $120\ kg$ equipment placed in a geostationary satellite, its weight will be mg' $= 120 \times 0.233$
$\Rightarrow26.76\approx27\text{N}$
We know that the value acceleration due to gravity above the surface of the Earth is given by $\text{g}'=\frac{\text{Gm}}{(\text{R + h})^2}.$
At h = 36000km, we have:$\text{g}'=\frac{\text{Gm}}{(36000+6400)^2}$
At the surface, we have:$\text{g}=\frac{\text{Gm}}{(6400)^2}$
$\therefore\frac{\text{g}'}{\text{g}}=\frac{6400\times6400}{42400\times42400}$
$=\frac{256}{106\times106}=0.0228$
$\Rightarrow\text{g}'=0.0227\times9.8=0.223 [$Taking $g = 9.8m/s^2$ at the surface of the earth$]$
For a $120\ kg$ equipment placed in a geostationary satellite, its weight will be mg' $= 120 \times 0.233$
$\Rightarrow26.76\approx27\text{N}$
