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.
Concept of Physics - 1 , HC VERMA , Chapter "The Force"
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Answered by
67
Hello Dear.
Given ⇒
Distance of the Geostationary Orbit from the Earth's Surface(h) = 36000 km.
Radius of the Earth(r) = 6400 km.
Total Distance between the Geostationary Orbit and the center of the Earth = h + r
= 36000 + 6400
= 42400 km.
We know, as the Height or the depth increases or decreases the value of the Acceleration due to gravity changes.
At Earth Surface,
Acceleration due to gravity = G m/r²
where, G = Gravitation Constant.
m = mass of the earth. and r = radius of the Earth.
∴ g = G m/(6400)²
G m = g × (6400)² ---------eq(i)
Now, At height (h+ r), the Acceleration due to gravity = G m/(h + r)²
g' = G m/(42400)²
∴ g' = g × (6400)² ÷ (42400)² [From eq(i)]
⇒ g' = g × 0.023
∵ g = 9.8 m/s².
∴ g' = 9.8 × 0.023
⇒ g' = 0.2254 m/s²
Hence, the Acceleration due to Gravity at the height (h + r) is 0.2254 m/s².
Mass of the Equipment placed in the Satellite = 120 kg.
∵ Weight = Mass × Acceleration due to gravity at that place.
∴ Weight = 120 × 0.2254
⇒ Weight = 27.048 N.
⇒ Weight ≈ 27 N.
Hence, the weight of the body placed in the Geostationary Satellite is 27 N.
Hope it helps.
Given ⇒
Distance of the Geostationary Orbit from the Earth's Surface(h) = 36000 km.
Radius of the Earth(r) = 6400 km.
Total Distance between the Geostationary Orbit and the center of the Earth = h + r
= 36000 + 6400
= 42400 km.
We know, as the Height or the depth increases or decreases the value of the Acceleration due to gravity changes.
At Earth Surface,
Acceleration due to gravity = G m/r²
where, G = Gravitation Constant.
m = mass of the earth. and r = radius of the Earth.
∴ g = G m/(6400)²
G m = g × (6400)² ---------eq(i)
Now, At height (h+ r), the Acceleration due to gravity = G m/(h + r)²
g' = G m/(42400)²
∴ g' = g × (6400)² ÷ (42400)² [From eq(i)]
⇒ g' = g × 0.023
∵ g = 9.8 m/s².
∴ g' = 9.8 × 0.023
⇒ g' = 0.2254 m/s²
Hence, the Acceleration due to Gravity at the height (h + r) is 0.2254 m/s².
Mass of the Equipment placed in the Satellite = 120 kg.
∵ Weight = Mass × Acceleration due to gravity at that place.
∴ Weight = 120 × 0.2254
⇒ Weight = 27.048 N.
⇒ Weight ≈ 27 N.
Hence, the weight of the body placed in the Geostationary Satellite is 27 N.
Hope it helps.
Answered by
16
HEY!!
______________________________
✔The geostationary orbit of the Earth is at a distance of about 36000 km.
✔Value of the acceleration due to the gravity above the surface of earth:- g'=Gm/(R+h)^2
▶At h = 36000 km, we have:-
g'=Gm/(36000+6400)^2
▶At surface, we have:-
g=Gm(6400)^2
▶▶g'/g= 6400×6400 / 42400×42400
256 / 106×106= 0.0228
✔g'= 0.0227× 9.8= 0.223
((Taking g=9.8 m/s2^2 at the surface of the earth))
✔For a 120 kg equipment placed in a geostationary satellite, its weight will be:-
▶mg' = 120 × 0.233
▶▶26.76 ≈ 27 N
______________________________
✔The geostationary orbit of the Earth is at a distance of about 36000 km.
✔Value of the acceleration due to the gravity above the surface of earth:- g'=Gm/(R+h)^2
▶At h = 36000 km, we have:-
g'=Gm/(36000+6400)^2
▶At surface, we have:-
g=Gm(6400)^2
▶▶g'/g= 6400×6400 / 42400×42400
256 / 106×106= 0.0228
✔g'= 0.0227× 9.8= 0.223
((Taking g=9.8 m/s2^2 at the surface of the earth))
✔For a 120 kg equipment placed in a geostationary satellite, its weight will be:-
▶mg' = 120 × 0.233
▶▶26.76 ≈ 27 N
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