✪ Physics ✪
The energy required to take a satellite to a height 'h' above earth surface (radius of earth = 6.4 × 10³ km) is E1 and kinetic energy required for the satellite to be in a circular orbit at this height is E2. The value of h for which E1 and E2 are equal is :-
a) 1.28 × 10⁴ km
b) 6.4 × 10³ km
c) 3.2 × 10³ km
d) 1.6 × 10³ km
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★Given :
- The energy required to take a satellite to a height 'h' above earth surface is E₁.
- Kinetic energy required for the satellite to be in a circular orbit at this height is E₂ .
- Radius of earth = 6.4 × 10³ km
★To find :
- The value of h for which E₁ and E₂ are equal
★Solution :
Applying conservation of total energy,
(K.E + P.E)₁ = (K.E + P.E)₂ __(1)
K.E of satellite is zero at the earth's surface.
And if we define the potential energy to be zero at r = infinity,U = -GmM/r.
Therefore,
We know :
Now,
Using the formula :
We have to find the value of h for which E₁ & E₂ are equal.Therefore,
Given that R = 6.4 × 10³ km.
Substituting this value in the above equation,
Therefore,
Option(C) is correct.
_____________
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