Gravitational Physics

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Newton's inverse-square force law

Fg=GM1M2r2F_g = \frac{GM_1 M_2}{r^2}

is elegant in its simplicity and leads to predictions qualitatively similar to observations, but it does not graduate to become a physical theory until ample quantitative data supports it.

In this quiz, we will investigate how scientists resolve theoretical models with experimental data. Specifically, we test the hypothesis that FgF_g is proportional to 1/r21/r^2 by examining a set of measurements of the orbital periods and radii of Jupiter's moons.

MoonOrbital periodT(106s)Orbital radiusR(106km)Io0.1530.422Europa0.3070.671Ganymede0.6181.070Callisto1.4421.883\begin{array}{c|c} \text{Moon} & \text{Orbital period}\,T\,(10^6 \si{\second}) & \text{Orbital radius}\,R\,(10^6 \si{\kilo\meter})\\ \hline \text{Io}& 0.153 & 0.422 \\ \text{Europa}& 0.307& 0.671 \\ \text{Ganymede}& 0.618& 1.070\\ \text{Callisto}& 1.442& 1.883 \\ \end{array}

In the next few questions we will

  • first, using Newton's gravitational force law, derive a relationship between orbital period and orbital radius for one of Jupiter's moons
  • then, perform a linear regression—the workhorse of 19th and 20th century science—which returns model parameters that most closely reproduces one variable as a function of the other.
             

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Possibly the most challenging step in validating a theoretical model with observational data is deciding on which data are most directly relevant. Here, we have basically identified that orbital radius and period are to be used as a test of Newton's gravitational law.

How Newton and concurrent astronomers whittled down all possible data to these two variables is too arduous to describe here. Clearly, directly measuring the force between Jupiter and any of its moon's is not feasible. It helped that these data are accessible to any patient astronomer with a decent telescope. Our task is to determine how Newton's gravitational law relates these variables.


The orbital period TT is how long it takes for one of Jupiter's moons to complete one revolution around the planet, but time does not appear explicitly in Fg.F_g. Modeling our approach on the last quiz where we related the Moon's centripetal acceleration to FgF_g let's look for a way to pull TT into this relationship.

If the orbital radius is RR which choice expresses centripetal acceleration ac=v2/Ra_c = v^2/R in terms of TT?

             

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According to the result of the last quiz, we suspect that Fg1/r2F_g\propto 1/r^2 but we would like to assess whether data from Jupiter's moons supports the same theory.

Thus, let's introduce a parameter ϵ\epsilon into the force law

Fg=GmmoonMJup.r2+ϵF_g=\frac{Gm_\text{moon}M_\text{Jup.}}{r^{2+\epsilon}}

expressing the deviation of the power law from an inverse-square law. We will use the data to estimate ϵ.\epsilon. The closer ϵ\epsilon is to 0,0, then the stronger the support for Newton's inverse-square law.


Using the result of the previous question, and Newton's second law, which choice expresses orbital period TT in terms of orbital radius RR?

Details

  • For a moon in a circular orbit, Fg=mmoonacF_g=m_\text{moon} a_cAssume the moons' orbits are circular and their motion is uniform.
             

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In a linear regression, the calculated parameters are the slope and intercept of a line that best fits a set of data.

Plotting the natural log (ln)(\ln) of period TT and orbital radius RR of the moon data, they fall almost exactly on a line. The slope and intercept of the best fit line are shown next to the plot.

Taking the natural log of your model relationship between TT and RR in the previous problem, what is the order of magnitude of the derivation ϵ\epsilon?

             

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Given that Jupiter's mass is 1.898×1027 kg\SI{1.898e27}{\kilo\gram}, make a prediction for proportionality constant GG from this data. The accepted value of the proportionality constant in Newtonian gravity is G=6.67408×1011 m3/(kgs2).G=\SI[per-mode=symbol]{6.67408e-11}{\meter\cubed\per\kilo\gram\per\second\squared}. By what fraction does the predicted value deviate from the accepted value?

Calculate GmeasuredGG.\frac{\lvert G_\text{measured}-G \rvert}{G}.

             

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Orbital data has been used over the last several centuries to validate Newton's universal law of gravity between massive bodies, as well as to validate its only known improvement (general relativity). Here, we've used it to narrow down the functional form of gravity to within one part in 10000\num{10000} of the exponent on r.r.

We can summarize our findings as follows:

Newtonian gravity is defined by the force law F=Gm1m2r2,F = G \frac{m_1 m_2}{r^2}, where rr is the magnitude of the displacement of the centers of two masses m1m_1 and m2,m_2, with G=6.67×1011 m3kg1s2.G=\SI{6.67e-11}{\meter\cubed\per\kilo\gram\per\second\squared}. The force between the masses is always attractive, directed between the centers of m1m_1 and m2.m_2.

             

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Newton's work unearthed the connection between falling objects and orbital motion. His theory formed the foundation of orbital mechanics, more than 250 years before the first man-made object was launched into orbit in 1957. Today, with more than 2,000 man-made satellites in orbit around Earth (and even more space junk), Newton's theory remains more relevant today than ever.

Newton's theory withstands the test of time because it exemplifies a bedrock assumption of modern science: that the laws of nature are systematic and universal, which was not a widely held belief in his time.

             
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