A rocket is fired vertically with a speed of 5 km s⁻¹ from the earth's surface. How far from the earth does the rocket go before returning to the earth mass of the earth? (Gravitational constant G = 6.67 × 10⁻¹¹ N m² kg⁻² , mean radius of the earth R = 6400 km, mass of the earth m = 6 × 10²⁴ kg.)
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Given, velocity of the rocket, v = 5 km/s = 5 × 10³m/s
Mass of the Earth, Me = 6 × 10²⁴ kg
Radius of the Earth, Re = 6.4 × 10^6 m
Height reached by rocket mass, m = h
At the surface of the Earth,
Total energy of the rocket = Kinetic energy + Potential energy
= (1/2)mv² + (-GmMe/Re)
At highest point h,
v = 0
And, Potential energy = -GmMe / (Re + h)
Total energy of the rocket = kinetic energy + potential energy
= 0 + [ -GmMe / (Re+ h) ]
= -GmMe / (Re + h)
From the law of conservation of energy,
total energy of the rocket at the Earth’s surface = Total energy at height h
1/2mv² + -GmMe/Re = -GmMe/(Re + h)
1/2v² = GMe [ (1/Re) – 1 / (Re + h) ]
= GMe[ (Re + h – Re) / Re(Re+ h) ]
(1/2)v² = ghRe / (Re + h)
Where g = GM / Re²
∴ v² (Re + h) = 2ghRe
v²Re = h(2gRe – v²)
h = Rev² / (2gRe – v²)
now putting , Re, v , g values
= 6.4 × 10^6 × (5 × 10³)²/[2 × 9.8 × 6.4 × 10^6 – (5 × 10³)²]
h = 1.6 × 10^6 m
Hence, Height achieved by the rocket with respect to the centre of the Earth = Re + h
= 6.4 × 10^6 + 1.6 × 10^6 = 8 × 10^6 m.
Mass of the Earth, Me = 6 × 10²⁴ kg
Radius of the Earth, Re = 6.4 × 10^6 m
Height reached by rocket mass, m = h
At the surface of the Earth,
Total energy of the rocket = Kinetic energy + Potential energy
= (1/2)mv² + (-GmMe/Re)
At highest point h,
v = 0
And, Potential energy = -GmMe / (Re + h)
Total energy of the rocket = kinetic energy + potential energy
= 0 + [ -GmMe / (Re+ h) ]
= -GmMe / (Re + h)
From the law of conservation of energy,
total energy of the rocket at the Earth’s surface = Total energy at height h
1/2mv² + -GmMe/Re = -GmMe/(Re + h)
1/2v² = GMe [ (1/Re) – 1 / (Re + h) ]
= GMe[ (Re + h – Re) / Re(Re+ h) ]
(1/2)v² = ghRe / (Re + h)
Where g = GM / Re²
∴ v² (Re + h) = 2ghRe
v²Re = h(2gRe – v²)
h = Rev² / (2gRe – v²)
now putting , Re, v , g values
= 6.4 × 10^6 × (5 × 10³)²/[2 × 9.8 × 6.4 × 10^6 – (5 × 10³)²]
h = 1.6 × 10^6 m
Hence, Height achieved by the rocket with respect to the centre of the Earth = Re + h
= 6.4 × 10^6 + 1.6 × 10^6 = 8 × 10^6 m.
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