SUMMARY
The velocity of a satellite orbiting Earth at a distance R from the Earth's center can be derived using Newton's law of universal gravitation and centripetal force equations. The correct formula for the orbital velocity is v = sqrt(G*M/R), where G is the gravitational constant and M is the mass of the Earth. The assumption of constant gravitational acceleration is incorrect for large distances, and the gravitational force must be expressed as Fg = G*m*M/d². This discussion clarifies the importance of using the correct variables and understanding the relationship between gravitational force and centripetal acceleration.
PREREQUISITES
- Understanding of Newton's law of universal gravitation
- Familiarity with centripetal force equations
- Knowledge of gravitational constant (G)
- Basic algebra for manipulating equations
NEXT STEPS
- Study the derivation of orbital mechanics using Newton's laws
- Learn about the implications of varying gravitational acceleration with distance
- Explore the concept of centripetal acceleration in different contexts
- Investigate the applications of satellite motion in real-world scenarios
USEFUL FOR
Students studying physics, aerospace engineers, and anyone interested in satellite dynamics and gravitational forces.