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MYP Physics · topic MYP-15.05

Circular motion and orbital systems

Connect the ideas, make your working visible, and test the result. Use the hints when you need a starting point; open the full solution after your attempt.

Extra challenging questions

Work through the linked stages and explain what each result means.

Extra challenging · 01

A satellite raised to twice the orbital radius

Optional enrichment: this challenge may extend beyond the usual syllabus depth and assumes confidence with algebra and graph interpretation. A spherical planet has radius R = 6.0×10⁶ m and surface gravitational field g₀ = 10 N kg⁻¹. A 100 kg satellite follows a circular orbit at radius 2R measured from the planet's centre. Ignore rotation and atmosphere. Use GM = g₀R² and the supplied inverse-square field data. Supplied model: Use g = GM/r², circular acceleration v²/r and orbital period T = 2πr/v. Supplied data (Radius / R; Field magnitude / N kg⁻¹): (1, 10), (2, 2.5), (3, 1.111111), (4, 0.625). (a) Find the satellite's weight, orbital speed and orbital period. Explain what supplies the centripetal resultant. [3 marks] (b) The radius is increased to 4R. Predict ratios of field, speed and period, and explain why astronauts can feel weightless despite nonzero gravity. [3 marks]

Explore the question data

Planetary gravitational field

Supplied question data. Read the labelled axes and use the observations to test the physical model.

Vertical axis (y): Field magnitude / N kg⁻¹

Planetary gravitational fieldSupplied question data. Read the labelled axes and use the observations to test the physical model. Horizontal axis: Radius / R. Vertical axis: Field magnitude / N kg⁻¹. Exact values are available in the data table below.02.557.51001234xy

Horizontal axis (x): Radius / R

Reading 1Radius / R: 1Field magnitude / N kg⁻¹: 10
Read the exact data as a table
Planetary gravitational field — supplied values
Radius / RField magnitude / N kg⁻¹
110
22.5
31.111111
40.625

These are the supplied values, not a worked answer. No fitted trend is drawn.

Show a hint

Begin with part (a): Find the satellite's weight, orbital speed and orbital period. Explain what supplies the centripetal resultant.

Reveal the worked solution
  1. At 2R the field is g₀/4 = 2.5 N kg⁻¹, so the gravitational force is mg = 250 N. The satellite's mass remains 100 kg.
  2. Gravity alone supplies mv²/r: v = √(gr) = √(2.5×1.2×10⁷)≈5477 m s⁻¹.
  3. Period is circumference/speed, T = 2πr/v≈1.38×10⁴ s. 'Centripetal force' names the inward resultant; it is not an additional interaction alongside gravity.
  4. For a circular orbit g∝r⁻², v∝r⁻¹/² and T∝r³/². Doubling r therefore gives the stated ratios.
  5. Astronauts and spacecraft accelerate together in free fall. Little support force acts on the astronauts, so their apparent weight can be near zero.
  6. The gravitational field is not zero in orbit, and constant speed still requires acceleration because velocity direction changes.

Answer (a) Weight = 250 N; orbital speed ≈5.48 km s⁻¹; period ≈1.38×10⁴ s. (b) Field becomes 1/4, speed 1/√2 and period 2√2 times the initial orbital values.

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