A rocket is fired from the earth towards the sun. At what distance from the earth’s centre is the gravitational force on the rocket zero ? Mass of the sun = 2×1030 kg, mass of the earth = 6×1024 kg. Neglect the effect of other planets etc. (orbital radius= 1.5 × 1011 m).
Mass of the Sun, Ms = 2 × 1030 kg
Mass of the Earth, Me = 6 × 10 24 kg
Orbital radius, r = 1.5 × 1011 m
Mass of the rocket = m
Let x be the distance from the centre of the Earth where the gravitational force acting on satellite P becomes zero.
From Newton’s law of gravitation, we can equate gravitational forces acting on satellite P under the influence of the Sun and the Earth as:
\(\frac{GmM_s}{ (r-x)^2}\) = Gm \(\frac{M_3}{x^2}\)
\((\frac{r-x}{x})^2 =\frac{ M_s}{ M_e}\)
\(\frac{r-x }{x} = (\frac{2 x 10^30 }{ 60 x 10^24 })^{ \frac{1}{2} }= 577.35\)
1.5 x 1011 -x = 577.35x
578.35x = 1.5 x 1011
\(x = \frac{1.5 x 10^11 }{ 578.35}\) = 2.59 x 108 m
Figures 9.20(a) and (b) refer to the steady flow of a (non-viscous) liquid. Which of the two figures is incorrect ? Why ?
Escape speed is the minimum speed, which is required by the object to escape from the gravitational influence of a plannet. Escape speed for Earth’s surface is 11,186 m/sec.
The formula for escape speed is given below:
ve = (2GM / r)1/2
where ,
ve = Escape Velocity
G = Universal Gravitational Constant
M = Mass of the body to be escaped from
r = Distance from the centre of the mass