•Discuss the importance of Newton’s Law of Universal Gravitation in understanding and calculating the motion of satellites.
basically it allowed us to understand the nature of the trajectory of the satellites, as it derived the concept of centripetal force and allowing us to describe the motions using conics (parabolic, hyperbolic...). This is based on the velocity of the object (or satellite) and its distance from the center of the more massive object (planet) as the acceleration or force is inversely proportional to distance squared (Newton's law of...). Also, as it provided understanding of the motion an object due to the attraction of a more massive object, it gave rise of obital velocity and escape velocity which is derived using equations... this was only made possible when the fact that centripetal force exists as without knowing this, it is impossible to even think about orbital velocity or escape velocity (u can just talk about the significance of orbital velocity and escape velocity now, eg. a velocity lower than orbital velocity=parabolic curve back to ground... and the equations of orbital velocity and escape velocity basically allows u to calculate the motion of the satellite for the same reason eg. lower than orbital velocity=parabolic path back to earth)
•Discuss the effect of the Earth’s orbital motion and its rotation motion on the launch of a rocket?
(i'm just writing the main points because i can't be bothered writing an essay on this and the points are not in order)
*earth rotates from west to east
*principle of relativity
*centrifuge effect
*max centrifuge effect at equator
*earth orbits around sun
*gravitational pull of earth on rocket
*vector addition