India’s Mangalyan was sent to the Mars by launching it into a transfer orbit EOM around the sun. It leaves the earth at E and meets Mars at M. If the semi-major axis of Earth’s orbit is ae = 1.51011 m, that of Mar’s orbit am = 2.28
1011 m, taken Kepler’s laws give the estimate of time for Mangalyan to reach Mars from Earth to be close to : (In days)
260
320
500
220
As we discussed in
Kepler's 3rd law -
From fig.
semi major Axis
Perigee
apogee
For EOM
time for Mangalyan to reach Mars from Earth=t=
So