AP®︎ Physics 1: Topic 6.6 Practice Test

Prepare for your quiz, test, or the AP exam with focused practice questions on Topic 6.6 of AP Physics 1 – Motion of Orbiting Satellites.


Questions List

Topic 6.6

Q1
Q2
Q3
Q4
Q5
Q6
Q7
Q8
Q9
Q10
Q11
Q12
Q13
Q14
Q15

Question 1 Easy

Earth orbits the Sun, whose mass is about 330,000 times Earth's mass. Consider only the gravitational interaction between Earth and the Sun.

Which of the following correctly compares the magnitudes of the gravitational forces the two objects exert on each other and the magnitudes of their accelerations?
A
Gravitational force magnitudesAcceleration magnitudes
The Sun's force on Earth equals Earth's force on the Sun.The Sun's acceleration equals Earth's.
B
Gravitational force magnitudesAcceleration magnitudes
The Sun's force on Earth is greater than Earth's force on the Sun.The Sun's acceleration is much smaller than Earth's.
C
Gravitational force magnitudesAcceleration magnitudes
The Sun's force on Earth is greater than Earth's force on the Sun.The Sun's acceleration equals Earth's.
D
Gravitational force magnitudesAcceleration magnitudes
The Sun's force on Earth equals Earth's force on the Sun.The Sun's acceleration is much smaller than Earth's.

What You’re Being Tested On:

Explore the learning objectives taken directly from the College Board’s AP® Physics 1 Curriculum. Ensure you’re prepared for the exact topics covered on the AP® exam, in-class tests, and quizzes, and gain confidence in your mastery of the material.

Topic 6.6: Motion of Orbiting Satellites

Learning Objective: 6.6.A

Describe the motions of a system consisting of two objects interacting only via gravitational forces.

Essential Knowledge: 6.6.A.1

In a system consisting only of a massive central object and an orbiting satellite with mass that is negligible in comparison to the central object’s mass, the motion of the central object itself is negligible.

Essential Knowledge: 6.6.A.2

The motion of satellites in orbits is constrained by conservation laws.

Essential Knowledge: 6.6.A.2.i

In circular orbits, the system’s total mechanical energy, the system’s gravitational potential energy, and the satellite’s angular momentum and kinetic energy are constant.

Essential Knowledge: 6.6.A.2.ii

In elliptical orbits, the system’s total mechanical energy and the satellite’s angular momentum are constant, but the system’s gravitational potential energy and the satellite’s kinetic energy can each change.

Essential Knowledge: 6.6.A.2.iii

The gravitational potential energy of a system consisting of a satellite and a massive central object is defined to be zero when the satellite is an infinite distance from the central object. Relevant equation: Ug=−Gm1m2rU_g = -G\frac{m_1m_2}{r}

Essential Knowledge: 6.6.A.3

The escape velocity of a satellite is the satellite’s velocity such that the mechanical energy of the satellite–central-object system is equal to zero.

Essential Knowledge: 6.6.A.3.i

When the only force exerted on a satellite is gravity from a central object, a satellite that reaches escape velocity will move away from the central body until its speed reaches zero at an infinite distance from the central body.

Essential Knowledge: 6.6.A.3.ii

The escape velocity of a satellite from a central body of mass M can be derived using conservation of energy laws. Derived equation: vesc=2GMrv_{\mathrm{esc}} = \sqrt{\frac{2GM}{r}}