Gravitation
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What is the direction of areal velocity of the earth around the sun?
What is the direction of areal velocity of the earth around the sun?
This is a Short Answer Type Questions as classified in NCERT Exemplar
Explanation-areal velocity of earth and sun
dA/dt=L/2m
where L is angular momentum
but we know L= r
dA/dt=1/2m (r )=1/2 (r )
so dA/dt direction will be perpendicular to the plane containing r and v
This is a Short Answer Type Questions as classified in NCERT Exemplar
Explanation-

areal velocity of a planet revolving around the sun is constant with respect to time.
Give one example each of central force and non-central force.
Give one example each of central force and non-central force.
Explanation- examples of central force – gravitational force and electrostatic force
Examples of non central force = nuclear force, magnetic force acting between two current carrying loops etc.
Molecules in air in the atmosphere are attracted by gravitational force of the earth. Explain why all of them do not fall into the earth just like an apple falling from a tree.
Molecules in air in the atmosphere are attracted by gravitational force of the earth. Explain why all of them do not fall into the earth just like an apple falling from a tree.
This is a Short Answer Type Questions as classified in NCERT Exemplar
Explanation-air molecules in the atmosphere are attracted vertically downward by the gravitational force of the earth just like an apple falling from the tree. Air molecules move randomly due to their thermal velocity and hen
A satellite is in an elliptic orbit around the earth with aphelion of 6R and perihelion of 2 R where R= 6400 km is the radius of the earth. Find eccentricity of the orbit. Find the velocity of the satellite at apogee and perigee. What should be done if this satellite has to be transferred to a circular orbit of radius 6R ? [G = 6.67 × 10–11 SI units and M = 6 × 1024 kg].
A satellite is in an elliptic orbit around the earth with aphelion of 6R and perihelion of 2 R where R= 6400 km is the radius of the earth. Find eccentricity of the orbit. Find the velocity of the satellite at apogee and perigee. What should be done if this satellite has to be transferred to a circular orbit of radius 6R ? [G = 6.67 × 10–11 SI units and M = 6 × 1024 kg].
This is a Long Type Questions as classified in NCERT Exemplar
Explanation- rp= radius of perihelion =2R
Ra = radius of aphelion =6R
So ra=a(1+e)=6R
And rp= a(1-e)=2R
Solving above eqns
We get e = ½
By conservation of angular momentum angular momentum at perigee= angular momentum at apogee
So mvpr
Earth’s orbit is an ellipse with eccentricity 0.0167. Thus, earth’s distance from the sun and speed as it moves around the sun varies from day to day. This means that the length of the solar day is not constant through the year. Assume that earth’s spin axis is normal to its orbital plane and find out the length of the shortest and the longest day. A day should be taken from noon to noon. Does this explain variation of length of the day during the year?
Earth’s orbit is an ellipse with eccentricity 0.0167. Thus, earth’s distance from the sun and speed as it moves around the sun varies from day to day. This means that the length of the solar day is not constant through the year. Assume that earth’s spin axis is normal to its orbital plane and find out the length of the shortest and the longest day. A day should be taken from noon to noon. Does this explain variation of length of the day during the year?
This is a Long Type Questions as classified in NCERT Exemplar
Explanation-let m be the mass of the earth vp, va be the velocity of the earth at perigee and apogee respectively. Similarly wp and wa are angular velocities.

At perigee, at apogee
If a is the semimajor axis of the earth's orbit then rp=a
A satellite is to be placed in equatorial geostationary orbit around earth for communication.
(a) Calculate height of such a satellite.
(b) Find out the minimum number of satellites that are needed to cover entire earth so that at least one satellites is visible from any point on the equator.
[M = 6 × 1024 kg, R = 6400 km, T = 24h, G = 6.67 × 10-11 SI units

A satellite is to be placed in equatorial geostationary orbit around earth for communication.
(a) Calculate height of such a satellite.
(b) Find out the minimum number of satellites that are needed to cover entire earth so that at least one satellites is visible from any point on the equator.
[M = 6 × 1024 kg, R = 6400 km, T = 24h, G = 6.67 × 10-11 SI units

Explanation- mass of earth M = 6
Radius of the earth , R = 6400km= 6.4
T=24h= 24
G = 6.67 10-11Nm2/kg2
(a) Time period T =
= 2
= ( )1/3
( )1/3-R
So after solving we get h = 3.59
(b) If satellite is at height h from the
Six point masses of mass m each are at the vertices of a regular hexagon of side l. Calculate the force on any of the masses.
Six point masses of mass m each are at the vertices of a regular hexagon of side l. Calculate the force on any of the masses.
This is a Long Type Questions as classified in NCERT Exemplar
Explanation- consider a diagram having vertices A,B,C,D,E and F

AC= AG+GC=2AG
= 2lcos300= 2l
=
AD=AH+HJ+JD= lsin300+l+lsin300=2l
Force on mass m at A due to mass m at B is f1= along AB
Force on mass m at A due to mass m at C is
A star like the sun has several bodies moving around it at different distances. Consider that all of them are moving in circular orbits. Let r be the distance of the body from the centre of the star and let its linear velocity be v, angular velocity ω, kinetic energy K, gravitational potential energy U, total energy E and angular momentum l. As the radius r of the orbit increases, determine which of the above quantities increase and which ones decrease.
A star like the sun has several bodies moving around it at different distances. Consider that all of them are moving in circular orbits. Let r be the distance of the body from the centre of the star and let its linear velocity be v, angular velocity ω, kinetic energy K, gravitational potential energy U, total energy E and angular momentum l. As the radius r of the orbit increases, determine which of the above quantities increase and which ones decrease.
This is a Long Type Questions as classified in NCERT Exemplar
Explanation- when a body og mass m is revolving around a star of mass M.

Linear velocity of the body v= so when r increases then v decreases.
Angular velocity of the body w = 2
According to kepler’s law T2 r3
So T= kr3/
8.25 A rocket is fired ‘vertically’ from the surface of mars with a speed of 2 km s–1. If 20% of its initial energy is lost due to Martian atmospheric resistance, how far will the rocket go from the surface of mars before returning to it? Mass of mars = 6.4×1023 kg; radius of mars = 3395 km; G = 6.67×10-11 N m2 kg–2.
8.25 A rocket is fired ‘vertically’ from the surface of mars with a speed of 2 km s–1. If 20% of its initial energy is lost due to Martian atmospheric resistance, how far will the rocket go from the surface of mars before returning to it? Mass of mars = 6.4×1023 kg; radius of mars = 3395 km; G = 6.67×10-11 N m2 kg–2.
Initial kinetic energy of the rocket =
Initial potential energy of the rocket =
Total initial energy =
If 20% of initial kinetic energy is lost due to Martian atmosphere resistance, then only 80% of its kinetic energy helps in reaching a height
Total initial energy available = 0.8