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AP Physics 1 2.9 Circular Motion Overview

Connect circular paths and orbits to centripetal acceleration, inward net force, tangential speed, radius, and Kepler’s third law.

Syllabus
Effective Fall 2025
Course
AP Physics 1: Algebra-Based

Exam points

  • Use speed and radius to calculate centripetal acceleration and identify the inward net force.
  • Use Kepler’s third law to compare periods and radii of circular orbits around the same central body.

2.9 Circular Motion question 1

[Maximum number: 3]

(7 points, suggested time 13 minutes)
A block of mass M is released from rest at Point A, a height 6 R above the horizontal. After being released, the block slides down a track, as shown. When released from Point A, the block does not lose contact with the track at any point. Points B and C are located at the highest points of their respective circular loops, both of radius R. All frictional forces are negligible.

Figure for Question 2.9 Circular Motion question 1 — AP Physics 1: Algebra-Based

Diagram A shows an energy bar chart that represents the gravitational potential energy UgU_{g} of the block-Earth system and the kinetic energy K of the block at Point A, when the block is released from rest at height 6 R.

Question (a)

(a)

On the following dot that represents the block, draw and label the forces (not components) that are exerted on the block at the instant the block slides through Point C. Each force must be represented by a distinct arrow starting on, and pointing away from, the dot.

[ 2 ]

Question (b)

(b)

A student claims that 4 R is the minimum height of Point A, such that the block can slide through Point C without losing contact with the track after the block is released from rest. Briefly explain why this claim is incorrect.

Figure 1

Figure 1

[ 1 ]

2.9 Circular Motion question 2

[Maximum number: 5]
Figure for Question 2.9 Circular Motion question 2 — AP Physics 1: Algebra-Based

(7 points, suggested time 13 minutes)

A spacecraft of mass m is in a clockwise circular orbit of radius R around Earth, as shown in the figure above. The mass of Earth is MEM_{E}.

Question (a)

(a)

Derive an equation for the orbital period T of the spacecraft in terms of m,ME,Rm, M_{E}, R, and physical constants, as appropriate. If you need to draw anything other than what you have shown in part (a) to assist in your solution, use the space below. Do NOT add anything to the figure in part (a).

[ 4 ]

Question (i)

(i)

Derive an equation for the orbital period T of the spacecraft in terms of m,ME,Rm, M_{E}, R, and physical constants, as appropriate. If you need to draw anything other than what you have shown in part (a) to assist in your solution, use the space below. Do NOT add anything to the figure in part (a).

[ 3 ]

Question (ii)

(ii)

A second spacecraft of mass 2 m is placed in a circular orbit with the same radius R. Is the orbital period of the second spacecraft greater than, less than, or equal to the orbital period of the first spacecraft? Greater than Less than Equal to
Briefly explain your reasoning.

[ 1 ]

Question (b)

(b)

The first spacecraft is moved into a new circular orbit that has a radius greater than R, as shown in the figure below.

Figure for Question (b) — AP Physics 1: Algebra-Based

Note: Figure not drawn to scale.
Is the speed of the spacecraft in the new orbit greater than, less than, or equal to the original speed? Greater than Less than Equal to
Briefly explain your reasoning.

[ 1 ]
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