A spaceship orbits around a planet at a height of 20 km from its surface. Assuming that only gravitational field of the planet acts on the spaceshop. What will be the number of complete revolutions made by the spaceship in 24 hours around the planet?
[Given mass of plane `=8xx10^(22)kg`
Radius of planet `=2xx10^(6)m`
Gravitational constant `G=6.67xx10^(-11)Nm^(2)//kg^(2)`]
A spaceship orbits around a planet at a height of 20 km from its surface. Assuming that only gravitational field of the planet acts on the spaceshop. What will be the number of complete revolutions made by the spaceship in 24 hours around the planet?
[Given mass of plane `=8xx10^(22)kg`
Radius of planet `=2xx10^(6)m`
Gravitational constant `G=6.67xx10^(-11)Nm^(2)//kg^(2)`]
[Given mass of plane `=8xx10^(22)kg`
Radius of planet `=2xx10^(6)m`
Gravitational constant `G=6.67xx10^(-11)Nm^(2)//kg^(2)`]
A
9
B
17
C
13
D
11
Text Solution
AI Generated Solution
The correct Answer is:
To solve the problem of finding the number of complete revolutions made by a spaceship in 24 hours around a planet, we will follow these steps:
### Step 1: Understand the Problem
The spaceship is orbiting at a height of 20 km above the surface of a planet with a radius of \(2 \times 10^6\) m. We need to calculate how many complete revolutions it makes in 24 hours.
### Step 2: Calculate the Total Radius of Orbit
The total radius \(r\) of the orbit is the sum of the radius of the planet \(R\) and the height \(h\) of the orbit:
\[
r = R + h
\]
Given:
- \(R = 2 \times 10^6 \, \text{m}\)
- \(h = 20 \, \text{km} = 20 \times 10^3 \, \text{m}\)
Calculating \(r\):
\[
r = 2 \times 10^6 \, \text{m} + 20 \times 10^3 \, \text{m} = 2.02 \times 10^6 \, \text{m}
\]
### Step 3: Calculate the Gravitational Force and Centripetal Force
Using the formula for gravitational force:
\[
F_g = \frac{G M m}{r^2}
\]
And the centripetal force required for circular motion:
\[
F_c = \frac{m v^2}{r}
\]
Setting \(F_g = F_c\):
\[
\frac{G M m}{r^2} = \frac{m v^2}{r}
\]
Cancelling \(m\) from both sides and rearranging gives:
\[
v^2 = \frac{G M}{r}
\]
### Step 4: Calculate the Velocity \(v\)
Taking the square root:
\[
v = \sqrt{\frac{G M}{r}}
\]
Where:
- \(G = 6.67 \times 10^{-11} \, \text{N m}^2/\text{kg}^2\)
- \(M = 8 \times 10^{22} \, \text{kg}\)
Substituting the values:
\[
v = \sqrt{\frac{6.67 \times 10^{-11} \times 8 \times 10^{22}}{2.02 \times 10^6}}
\]
### Step 5: Calculate the Time Period \(T\)
The time period \(T\) of the orbit can be calculated using:
\[
T = \frac{2 \pi r}{v}
\]
### Step 6: Calculate the Number of Revolutions in 24 Hours
The number of revolutions \(n\) in 24 hours is given by:
\[
n = \frac{T_{\text{total}}}{T}
\]
Where \(T_{\text{total}} = 24 \times 3600 \, \text{s}\).
### Step 7: Substitute and Solve
1. Calculate \(v\) using the values from Step 4.
2. Calculate \(T\) using the value of \(v\) from Step 5.
3. Finally, calculate \(n\) using the total time in seconds from Step 6.
### Final Calculation
After performing all calculations, we find that the number of complete revolutions \(n\) is approximately 11.
### Conclusion
The number of complete revolutions made by the spaceship in 24 hours around the planet is **11**.
---
Topper's Solved these Questions
Similar Questions
Explore conceptually related problems
A synchronous satellite goes around the earth one in every 24 h. What is the radius of orbit of the synchronous satellite in terms of the earth's radius ? (Given: Mass of the earth , M_(E)=5.98xx10^(24) kg, radius of the earth, R_(E)=6.37xx10^(6)m , universal constant of gravitational , G=6.67xx10^(-11)Nm^(2)kg^(-2) )
Calculate the mass of sum if the mean radius of the earth's orbit is 1.5xx10^(8)km and G=6.67xx10^(-11)Nxxm^(2)//kg^(2)
Find the gravitational potential due to a body o fmass 10kg at a distance (i) 10m and (ii) 20 m from the body. Gravitational constant G = 6.67 xx 10^(-11) Nm^(2) kg^(-1) .
Calculate the escape velocity from the surface of a planet of mass 14.8 xx 10^(22) kg. It is given that radius of the planet is 3.48 xx 10^(6) m.
Calculat the binding energy of the - sum system . Mass of the earth =6xx 10 ^(24) kg , mass of the sun = 2 xx 10^(30) kg, distance between the earth and the sun = 1.5 xx 10^(11) and gravitational constant = 6.6 xx 10 ^(-11) N m^(2) kg^(2)
A Satellite is revolving around a planet having mass M=8xx10^(22)kg and radius R=2xx10^(6)m as shown in figure. Find the number of revolutions made by the satellite around the planet in 24 hours.
What is the magnitude of the gravitational force between the Earth and a 1kg object on its surface ? (Mass of the earth is 6xx10^(24) kg and radius of the Earth is 6.4xx10^(6) m) .
A planet has a mass of 2.4xx10^(26) kg with a diameter of 3xx10^(8) m. What will be the acceleration due to gravity on that planet ?
Calculate the escape speed on the surface of a planet of mass 7.5xx10^(25)g , and radius 1.6xx10^(8)cm. G=6.67xx10^(-8)"dyne"cm^(2)g^(-2) .
Calculate the velocity with which a body must be thrown vertically upward from the surface of the earth so that it may reach a height of 10R , where R is the radius of the earth and is equal to 6.4 xx 10^(6)m. (Given: Mass of the earth = 6 xx 10^(24) kg , gravitational constant G = 6.7 xx 10^(-11) N m^(2) kg^(-2) )