Question 1

What is critical velocity for a satellite in orbit?

Accepted Answer

Critical velocity is the specific horizontal velocity at which a satellite follows a perfectly circular orbit around Earth. At this velocity, the centripetal acceleration required for circular motion equals the acceleration due to gravity. Below this speed, the object falls to Earth; above it, the satellite enters an elliptical orbit instead of maintaining a circular path.

Question 2

How does centripetal acceleration relate to gravitational force in circular orbits?

Accepted Answer

In a circular satellite orbit, centripetal acceleration equals the acceleration due to gravity acting on the satellite. This equality ensures the gravitational force provides exactly the right inward pull to maintain circular motion. The satellite's weight continuously pulls it toward Earth while its tangential velocity keeps it moving forward, creating a stable circular path.

Question 3

What is the formula for calculating a satellite's critical velocity?

Accepted Answer

Critical velocity equals the square root of the product of the gravitational constant and Earth's mass divided by the satellite's total distance from Earth's center. This formula shows that critical velocity decreases with increasing orbital distance. Satellites closer to Earth require higher velocities to maintain circular orbits than those farther away.

Question 4

How does orbital velocity change with distance from Earth?

Accepted Answer

Orbital velocity decreases as distance from Earth increases. A satellite orbiting closer to Earth's surface needs higher speed to maintain a circular path than one orbiting farther away. This relationship follows from the inverse square law of gravitation and the requirement that gravitational force provides the necessary centripetal force for circular motion.

Question 5

What happens to a satellite's orbit if its velocity exceeds critical velocity?

Accepted Answer

When a satellite's velocity exceeds critical velocity, it no longer follows a circular path but instead enters an elliptical orbit around Earth. The excess velocity causes the satellite to move farther from Earth than it would in a circular orbit. Kepler's laws describe these elliptical orbital paths and their relationship to orbital period and distance.

Question 6

Why is a circular orbit the simplest type of orbit to analyze?

Accepted Answer

Circular orbits are the simplest to analyze because orbital speed and period calculations are straightforward when the satellite maintains constant distance from Earth's center. The uniform circular motion means constant velocity and acceleration, making mathematical relationships between speed, period, and orbital radius easier to derive and understand compared to elliptical orbits.

Question 7

How does tangential velocity determine whether an object orbits or falls to Earth?

Accepted Answer

Tangential velocity determines the object's forward motion while gravity pulls it downward. At critical velocity, Earth's surface curves away at the same rate the object falls toward it, creating a circular orbit. Below critical velocity, gravity pulls the object down faster than the surface curves, causing it to fall; above critical velocity, the object moves into an elliptical orbit.

衛星の円軌道と臨界速度