Eduqas A-Level Physics A420QS
Basic Physics
Kinematics
Dynamics
Energy Concepts
Circular Motion
Vibrations
Kinetic Theory
Thermal Physics
Conduction of Electricity
Resistance
D.C. Circuits
Capacitance
Solids Under Stress
Electrostatic and Gravitational Fields of Force
Using Radiation to Investigate Stars
Orbits and the Wider Universe
The Nature of Waves
Wave Properties
Refraction of Light
Photons
Lasers
Nuclear Decay
Particles and Nuclear Structure
Nuclear Energy
Magnetic Fields
Electromagnetic Induction
Option A: Alternating CurrentsOption A
Option B: Medical PhysicsOption B
Option C: The Physics of SportsOption C
Option D: Energy and the EnvironmentOption D
Mathematical Requirements (Appendix C)
Orbits and the Wider Universe
Newton's law of gravitation applied to planets and satellites
- 3 things to know
- Component 2
Overview
Recall questions on setting the gravitational force equal to the centripetal force, deriving the orbital speed, why the orbiting mass cancels, how speed varies with radius, and worked speed and period calculations for planets and satellites.
What you need to know
Answer each one before you reveal it.
What provides the centripetal force that keeps a planet in orbit around a star?
Write the condition for a body of mass m in a circular orbit of radius r about a mass M.
Questions from this subtopic
Each one with the model answer underneath.
- 1
Write Newton's law of gravitation in the form used for a planet of mass m orbiting a star of mass M, and state carefully what r represents.
Model answer
The law is F = GMm/r², with F in newtons, the masses in kilograms and G equal to 6.67 × 10⁻¹¹ N m² kg⁻². The distance r is measured between the centres of the two bodies, not from the surface of either.
- 2
What provides the centripetal force that keeps a planet in orbit around a star?
Model answer
The gravitational attraction between the star and the planet provides the centripetal force, directed towards the star at all times.
- 3
Write the condition for a body of mass m in a circular orbit of radius r about a mass M.
Model answer
The gravitational force equals the required centripetal force, so GMm/r² = mv²/r, where v is the orbital speed.
- 4
Derive an expression for the orbital speed of a satellite in a circular orbit of radius r about a mass M.
Model answer
Setting GMm/r² = mv²/r and cancelling m and one factor of r gives v² = GM/r, so v = √(GM/r).
- 5
Why is the mass of an orbiting satellite irrelevant to its orbital speed?
Model answer
The satellite's own mass appears on both sides of GMm/r² = mv²/r and cancels, so only the central mass and the orbital radius are left.
- 6
How does the orbital speed of a satellite change as the orbital radius increases?
Model answer
The speed decreases, because v = √(GM/r) makes it inversely proportional to the square root of the radius.
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