For elliptical orbits, in the equation refers to
radius of orbit
major axis
semi-minor axis
semi-major axis
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Kepler's third law states that the square of time period of revolution of a planet around the sun is directly proportional to the cube of semi-major axis of its elliptical orbit.
In planetary motion
the angular speed remains constant
the total angular momentum remains constant
the linear speed remains constant
neither the angular momentum nor angular speed remains constant
In planetary motion, there is no external torque. Hence from the equation , if constant
Kepler's second law may be stated as "under the influence of central force, in equal interval of time, position vector sweeps out equal
distance
area
displacement
volume
Angular momentum of the planet about is conserved. So, constant.
is maximum when is minimum.
So, is maximum at point . Hence K.E. is maximum at .
A planet revolves about the sun in elliptical orbit. The areal velocity of the planet is . The least distance between planet and the sun is . Then the maximum speed of the planet in is
10
20
30
40
angular momentum)
In planetary motion the areal velocity of position vector of a planet depends on angular velocity and the distance of the planet from sun . If so, the correct relation for areal velocity is
Which of the following astronomers proposed a definitive model in which the planets moved in circles around a fixed central sun?
Copernicus
Kepler
Galileo
None of these
A planet goes round the sun three times as fast as the earth. If and are the radii of orbit of the planet and the earth respectively then
The maximum and minimum distances of a comet from the sun are and . If its velocity when nearest to the sun is , what will be its velocity in when it is farthest
12
60
112
6
By law of conservation of angular momentum, constant
The period of moon's rotation around the earth is nearly 29 days. If moon's mass were 2 fold its present value and all other things remain unchanged, the period of moon's rotation would be nearly
days
29 days
Time period does not depend upon the mass of satellite.
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