A particle is projected from the surface of the earth (of radius R and mass M) with speed V given by
V = R G M at a certain angle from the local horizantal as shown in the figure such that the angle subtended by arc between launching and landing site at earth's centre is β = 2 π
Maximum separation of the particle from the centre of the earth is xR. find ⌊ 1 0 x ⌋
Consider the earth to be uniformly dense and air resistance to be absent.
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The speed of 8 km/ s or Sqrt (GM/ R), if arrived to parking orbit, then it cannot persist at the speed for circular motion at relatively low angular speed. How can we know that there will be an elliptical path at a lower level of higher angular speed?
How T.E = -GMm /2a ?
@Thomas Jacob , Bhai, Mein teko bola tha na, T.E ka formula. Haha :P , Tu mann ni raha tha :P
Let the length of semimajor axis be a and eccentricity of the ellipse be e 2 R − G M m + 2 m ( R G M ) 2 = − 2 a G M m
a = R As the separation between the ends of semi-major minor axis and the focus is equal to the length of the semi major axis we can clearly say that launching and landing sites are at the end of the semi minor axis. R c o s 4 π = a e
a + a e = R 2 2 + 1
Two typos R instead of 2R in eq of energy
Can you please explain how did you find eccentricity
The height wanted was on the Ap-vertex (not Peri-vetex) with mass point earth situated on a far focus of the ellipse. Mass point has been a usual practice for people to consider calculations in Physics or Mechanics like this.
Think about the earth revolving about the sun in a circle. Imagine that the sun split into two equal mass and moving apart from each other gradually. Assuming that they do not collide with the earth and eventually situated outside the original circle, would the earth is still revolving about that circle?
The center of mass of the sun is unchanged according to calculation. Before getting out-sided, would you think that the earth shall see no difference but just to keep on with the same circle?
Can you tell at what criteria of speed example Sqrt (G M / R) for this question that we can calculate with ellipse as described? Is this an estimation or a precise calculation?
Maybe you can switch this image in place of the one posted now, which is hard to discern.
Edit Okay, it's been switched. All good.
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This is really a beautiful problem. This uses a bit of knowledge of mathematics too. Solve this problem if you are comfortable of properties of ellipses. Let us calculate the total energy of the particle at the time of launch. T E = K E + P E T E = 2 m R G M − R G M m T E = 2 R − G M m We know that the particle will move around in an orbit of ellipse. Let eccentricity and semi major axis and semi minor axis of the ellipse are e and a and b respectively. Now it is well known that T E = 2 a − G M m Hence we get a = R We know that Center of Earth will lie on one of the focii of the ellipse. Also if we draw the line joining end of minor axis and the focus the length of the segment is a . So we can say that if we join the point of launch and point of landing, that would be semi minor axis. From geometry and pythagoras theorem we get 2 b = 2 R Hence b = 2 R From geometry of ellipse e 2 = 1 − a 2 b 2 e = 2 1 Again from geometry of ellipse, length of focus from far off vertex is d = a + a e Hence d = R ( 1 + 2 1 )