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Theme D — Fields

D.1.11 Orbital Motion, Speed and Energy — IB Physics HL Revision Notes & Topical Questions

5 min read 10 parts Lesson 13 of 39 1 quiz

📚 IB Physics HL Hub / Topical Revision
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Curriculum Equation Key قوانين الرقم الهيدروجيني والاتزان الأيوني - pH & Acid-Base Equilibrium FormulasFast Exam Solution
pH = -log[H⁺] | pOH = -log[OH⁻] | pH + pOH = 14 | [H⁺][OH⁻] = 10⁻¹⁴
Word Equation & Conditions: الرقم الهيدروجيني = -لوغاريتم تركيز أيون الهيدروجين | pH + pOH = 14
Location & Specifications: الاتزان الأيوني، كيمياء 3 ثانوي، التحصيلي، و AP Chemistry.
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Lesson summary

D.1.11 Orbital Motion, Speed and Energy — IB PHYSICS HL notes: Derive orbital speed from gravity as the centripetal force and use the kinetic, potential and total energy of a satellite.Near-circular orbits — the gravitational force between planet and star, or planet and satellite…

  • Mass cancels
  • Larger orbits
  • Acceleration
  • Kepler's third law
  • Geostationary orbit
  • Projectile picture

Part 1 of 8Gravity as the centripetal force

Near-circular orbits
  • Near-circular orbits the gravitational force between planet and star, or planet and satellite, provides the centripetal force
Direction
  • Direction both forces are perpendicular to the direction of travel
Equation
  • GMm/r2 = mv2/r
Free fall
  • Free fall the satellite is in constant free fall around the planet

Part 2 of 8Orbital speed

Equation
  • Equation v = √(GM/r)
Mass cancels
  • Mass cancels all satellites at one radius travel at the same speed
Symbols
  • M is the larger mass in kg, r the orbital radius from the centre in m
Larger orbits
  • Larger orbits smaller speed
Acceleration
  • Acceleration the centripetal acceleration points towards the planet

Part 3 of 8Orbital period

Period
  • T = 2πr/v = 2π√(r3/GM)
Kepler's third law
  • T2 = 4π2r3/GM so T2 ∝ r3
Geostationary orbit
  • Geostationary orbit period 24 h above the equator, fixed over one longitude

Part 4 of 8Weightlessness

Gravity
  • Gravity it has not vanished, and at the space station's height the field is about 89% of the surface value
Free fall
  • Free fall the astronaut and station fall together with the same acceleration, so there is no contact force
Projectile picture
  • Projectile picture a satellite is a projectile fired fast enough that the Earth's surface curves away as quickly as it falls

Part 5 of 8Energy of an orbiting satellite

Kinetic energy
  • Ek = ½mv2 = GMm/2r
    What the symbols mean: Ek = kinetic energy (J) · m = mass (kg) · v = speed (m s−1)
Potential energy
  • Ep = −GMm/r
Total energy
  • E = Ek + Ep = −GMm/2r
Relations
  • Ek = −E and Ep = 2E
Bound
  • Bound the negative total energy shows the satellite is bound
Constant
  • Constant in a given orbit Ek, Ep and E are constant

Part 6 of 8Comparing orbits

QuantitySmaller orbit XLarger orbit Y
Gravitational forceLargerSmaller
SpeedHigherLower
Kinetic energyHigherLower
Potential energyLowerHigher
PeriodShorterLonger
Raising an orbit
  • Raising an orbit engines must increase the total energy and the satellite ends up moving more slowly
Scaling
  • Scaling v ∝ r−1/2, T ∝ r3/2 and Ek ∝ 1/r

Part 7 of 8Energy graphs

Ep
  • Ep below the axis and rising towards zero with r
Ek
  • Ek positive and falling towards zero
Total energy
  • Total energy lies halfway between them, negative and rising to zero
v2 against 1/r
  • v2 against 1/r a straight line through the origin with gradient GM

Part 8 of 8More from the specification

More from the specification
Orbital speed relation
  • Orbital speed relation balancing centripetal requirements against gravitational force provides a direct physical means to determine orbital velocity.
Gravitational Field Strength Definition
  • Gravitational field strength g at a point in space is defined as the gravitational force per unit test mass placed at that position (g = F / m), directed along field lines toward the attracting centre.
Escape Speed from a Celestial Object
  • Escape speed is the minimum initial launch speed needed for an object to overcome the gravitational field strength of a planet without additional thrust, given by vesc = √(2GM / R).
Gravitational Potential Graphs
  • On a graph of gravitational potential V against distance r, the field is non-uniform (V = -GM/r);
    • the negative gradient (-dV/dr) at any point equals the local gravitational field strength g.
Escape velocity
  • Minimum speed to escape a planet's gravity without further propulsion; about 11.2 km/s for Earth.
Distance
  • Total length of path travelled, a scalar.
Uniform
  • Same density throughout, so the weight acts at the centre.
Newton
  • Unit of force, kg m s-2.
Density
  • Mass per unit volume.
Equipotential
  • A surface of constant potential
Field strength
  • G = Fg/m.
Field lines
  • Lines showing the direction and strength of a magnetic field.
Escape speed
  • Minimum launch speed to reach infinity, √(2GM/R).

Key terms

TermMeaning
Orbital speedv = √(GM/r), the speed of a circular orbit.
Centripetal forceThe inward force required for circular motion, here supplied by gravity.
Geostationary orbitAn equatorial orbit with a 24 h period so the satellite stays above one point.
Free fallMotion under gravity alone, giving apparent weightlessness.
Total orbital energy−GMm/2r.

Avoid these mistakes

1
Believing orbiting astronauts are beyond the pull of gravity.
2
Using the satellite's mass in the orbital speed formula — it cancels.
3
Saying a higher orbit needs a higher speed — the speed is lower.
4
Giving a positive total energy for a bound orbit.
5
Measuring r from the surface instead of the centre.

Last updated:

Physics 0625 & 9702 SUVAT Mastery Graph Interpretation

Constant Acceleration Equations (SUVAT) & Slopes

v = u + at  |  s = ut + ½at2  |  v2 = u2 + 2as  |  s = ½(u + v)t

  • Displacement-Time Graph: Gradient = Velocity (curve = accelerating).
  • Velocity-Time Graph: Gradient = Acceleration; Area under curve = Distance travelled / Displacement.
  • Free Fall in vacuum: a = g ≈ 9.81 m/s2 downwards (air resistance negligible).
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