Why do astronauts float and how are orbital periods related to radius?
Explain apparent weightlessness and apply Kepler's laws to the orbits of satellites and planets.
Apparent weightlessness as free fall, the difference between low Earth and geostationary orbits, and Kepler's three laws including the link between period and orbital radius.
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What this dot point is asking
This dot point applies gravity and circular motion to real orbits, and explains the often misunderstood idea of weightlessness in space.
Apparent weightlessness
Weight is the gravitational force , and it does not disappear in orbit. At the altitude of the International Space Station, gravity is still about 90 per cent of its surface value. What changes is the apparent weight, which is the normal force a surface pushes back with.
In orbit the station and everything in it are in continuous free fall toward Earth, accelerating at the local . Because the floor falls with the astronaut, it pushes with zero normal force, and with no normal force there is nothing to sense as weight. This is true weightlessness only in deep space far from any mass; in orbit it is apparent weightlessness caused by free fall.
Low Earth and geostationary orbits
The orbital speed shows that lower orbits are faster. A low Earth orbit has a period of about 90 minutes. A geostationary orbit is special: its period is exactly one sidereal day, so the satellite stays above a fixed point on the equator, ideal for communications. Setting in Kepler's third law gives a radius of about , roughly 36000 km above the surface.
Kepler's three laws
Kepler described planetary orbits before Newton explained them:
- The law of ellipses: each planet moves in an ellipse with the Sun at one focus. For most school problems we approximate orbits as circles.
- The law of equal areas: a line from the Sun to a planet sweeps out equal areas in equal times, so a planet moves faster when closer to the Sun.
- The law of periods: the square of the orbital period is proportional to the cube of the orbital radius.
The third law follows directly from equating gravity to the centripetal force:
so is the same constant for every satellite of a given central body, and you can compare two orbits without knowing or .
In the exam, when comparing orbits use Kepler's third law as a ratio so the unknown constants drop out. When asked about weightlessness, state clearly that gravity still acts and that the sensation comes from the absence of a normal force during free fall.
Exam-style practice questions
Practice questions written in the style of TASC exam questions on this dot point, with worked answer explainers. The year tag is the paper they imitate, not the source.
2019 TASC5 marksAstronomers study the star S2 orbiting an invisible object SgrA* at the centre of our Galaxy. Assume its orbit is circular with period 16.1 years and radius 1.30 x 10^14 m. Find the average speed of S2 (in km/s) and the mass of the invisible object SgrA*.Show worked answer →
Average speed is the circumference divided by the period:
T = 16.1 x 3.156 x 10^7 = 5.08 x 10^8 s.
v = 2 pi r / T = 2 pi x 1.30 x 10^14 / 5.08 x 10^8 = 8.17 x 10^14 / 5.08 x 10^8 = 1.61 x 10^6 m s-1 = 1610 km/s.
Mass of SgrA* from gravity providing the centripetal force, M = v^2 r / G:
M = (1.61 x 10^6)^2 x 1.30 x 10^14 / 6.67 x 10^-11
= 2.59 x 10^12 x 1.30 x 10^14 / 6.67 x 10^-11
= 3.37 x 10^26 / 6.67 x 10^-11 = 5.05 x 10^36 kg.
The central object is about 5 x 10^36 kg (roughly 2.5 million Suns), consistent with a supermassive black hole. Markers want v = 2 pi r / T then M = v^2 r / G.
2023 TASC3 marksAn exoplanet 'b' orbits its star with period 1.62 Earth days. A second planet 'c' has an orbital radius 1.21 times that of Earth's orbit around its own star. Using Kepler's third law, calculate the orbital period of 'c' in Earth days, given that 'b' orbits at the radius found earlier.Show worked answer →
Kepler's third law states T^2 is proportional to r^3 for bodies orbiting the same star: T_c^2 / T_b^2 = (r_c / r_b)^3.
Using the worked radius of planet 'b' (about 4.11 x 10^9 m) and r_c = 1.21 x 1.50 x 10^11 = 1.82 x 10^11 m:
(r_c / r_b)^3 = (1.82 x 10^11 / 4.11 x 10^9)^3 = (44.2)^3 = 8.65 x 10^4.
T_c^2 = T_b^2 x 8.65 x 10^4 = (1.62)^2 x 8.65 x 10^4 = 2.62 x 8.65 x 10^4 = 2.27 x 10^5.
T_c = 476 Earth days.
Markers reward applying T^2 proportional to r^3 with a consistent reference orbit and quoting the answer in days.
2024 TASC3 marksA planet exists at an orbital radius of 9.0 x 10^10 m from a neutron star of mass 2.79 x 10^30 kg. Calculate the orbital period of the planet, in Earth days.Show worked answer →
Gravity provides the centripetal force, giving Kepler's third law: T^2 = 4 pi^2 r^3 / (G M).
T^2 = 4 pi^2 x (9.0 x 10^10)^3 / (6.67 x 10^-11 x 2.79 x 10^30)
= 39.48 x 7.29 x 10^32 / (1.861 x 10^20)
= 2.878 x 10^34 / 1.861 x 10^20 = 1.547 x 10^14.
T = sqrt(1.547 x 10^14) = 1.244 x 10^7 s.
Convert to days: 1.244 x 10^7 / 86400 = 144 Earth days.
The planet orbits in about 144 days. Markers want T^2 = 4 pi^2 r^3 / GM and the conversion of seconds to days.