One method of identifying planets orbiting distant stars is by observing the planet passing in front of the star (known as a "transit"). You observe two of these transits exactly 247 days apart. Using the brightness and color of the star, you estimate its mass to be 8 × 1030 kg. At what distance from the star does the planet orbit? You will need to know the gravitational constant, G = 6.67x10-11 m3kg−1s−2. You may assume the planet orbits in a circle and is much lighter than the star.

Respuesta :

Given Information:

Time period = T = 247 days

Mass of planet = M =  8×10³⁰ kg

Required Information:

Distance from star = r = ?

Answer:

Distance from star = r = 1.833×10¹¹ m

Explanation:

We know that time period is given by

[tex]T = 2\pi \sqrt{\frac{r^{3}}{GM} }[/tex]

Where r is the distance from the star that we want to find out, M is the mass of the planet and G is the gravitational constant.

G = 6.6743×10⁻¹¹ m³/kg⋅s²

[tex]T = 2\pi \sqrt{\frac{r^{3}}{GM} }\\\\\frac{T}{2\pi} = \sqrt{\frac{r^{3}}{GM} }\\\\(\frac{T}{2\pi})^{2} = (\sqrt{\frac{r^{3}}{GM} })^{2} \\\\(\frac{T}{2\pi})^{2} = \frac{r^{3}}{GM} } \\\\r^{3} = (\frac{T}{2\pi})^{2} \cdot GM\\\\r = \sqrt[3]{((\frac{T}{2\pi})^{2} \cdot GM)}[/tex]

Convert time from days into seconds

Each day has 24 hours, each hour has 60 minutes, each minute has 60 seconds

T = 247*24*60*60

T = 2.134×10⁷ s

Substitute the given values

[tex]r = \sqrt[3]{((\frac{2.134\times 10^{7}}{2\pi})^{2} \cdot 6.6743\times 10^{-11}\cdot 8\times 10^{30})}\\\\r = 1.833\times 10^{-11} \: m[/tex]

Therefore, the planet is orbiting at a distance of 1.833×10¹¹ m from the star.

Answer:

 r=  1.83 10¹¹ m

Explanation:

For this exercise we use Newton's second law where the force is the force of universal attraction

             F = m a

             F = G m M / r²

acceleration is centripet

            a = v² / r

we substitute

           G m M /r² = m v² / r

            G M  /r = v2

Since the orbit is circular, the speed (modulus of speed) is constant, so we can use the uniform motion relation

          v = d / t

the distance traveled in the orbit is equal to the length of the circle

          d = 2π r

the time in this case is called period (T)

          v = 2π r / T

we substitute

             G M /r = 4π²  r² / T²

              r³ =  G M T²/4π²  

reduce the period to SI units

             T = 247 d (24h / 1d) 3600 s / 1h) = 2,134 107 s

let's calculate

             r³ =   6.67 10⁻¹¹ 8 10³⁰ (2,134 10⁷)²/ (4π²)

             r =∛( 6.155  10³³)

             r=  1.83 10¹¹ m