Make a chart of the descending plan of Chandr

Explain the descending plan along with the chart

Case studies

Study about the columbia space shuttle disaster in 2003 and the Discovery disaster in 1986

Assignment 3

An artificial Earth satellite is in an elliptical orbit which brings it to an altitude of 250 km at perigee and out to an altitude of 500 km at apogee. Evaluate the velocity of the satellite at both perigee and apogee. Evaluate the velocity change required to transfer a satellite from a circular 600 km orbit with an inclination of 28 degrees to an orbit of equal size with an inclination of 20 degrees. 2-body problem and their assumptions Orbit deviations due to injection errors. How are they rectified? (Refer my linkedin article post)

Assignment 2a

Write in two sentences for the following Applications of Libration points Relevance of Newton’s law of universal gravitation Assumptions of 2 body problem Stages of injection of satellite in its orbit Types of orbital perturbations Jacobi identity causes of orbital perturbations satellite transfer of orbit satellite injection