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A comet moves in an elliptical orbit wit...

A comet moves in an elliptical orbit with an eccentricity of e = 0.20 around a star. The distance between the perihelion and the aphelion is `1.0 xx 10^(8)` km. If the speed of the comet at perihelion is 81 km/s, then speed of the comet at the aphelion is :

A

182 km/s

B

36 km /s

C

121.5 km/s

D

54 km/s

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To solve the problem, we need to find the speed of the comet at aphelion given its speed at perihelion and the distance between the perihelion and aphelion. ### Step 1: Understand the terms - **Perihelion (r₁)**: The point in the orbit where the comet is closest to the star. - **Aphelion (r₂)**: The point in the orbit where the comet is farthest from the star. - The distance between perihelion and aphelion is given as \(1.0 \times 10^8\) km. ### Step 2: Relate perihelion and aphelion distances The distance between the perihelion and aphelion can be expressed as: \[ d = r_2 - r_1 \] where \(d\) is the distance between perihelion and aphelion. ### Step 3: Express perihelion and aphelion in terms of semi-major axis (a) and eccentricity (e) For an elliptical orbit: - The perihelion distance \(r_1 = a(1 - e)\) - The aphelion distance \(r_2 = a(1 + e)\) Thus, the distance between perihelion and aphelion can be expressed as: \[ d = r_2 - r_1 = a(1 + e) - a(1 - e) = 2ae \] ### Step 4: Solve for semi-major axis (a) Given that \(d = 1.0 \times 10^8\) km and \(e = 0.20\): \[ 1.0 \times 10^8 = 2a(0.20) \] \[ 1.0 \times 10^8 = 0.4a \] \[ a = \frac{1.0 \times 10^8}{0.4} = 2.5 \times 10^8 \text{ km} \] ### Step 5: Calculate perihelion and aphelion distances Now we can find \(r_1\) and \(r_2\): \[ r_1 = a(1 - e) = 2.5 \times 10^8 (1 - 0.20) = 2.5 \times 10^8 \times 0.80 = 2.0 \times 10^8 \text{ km} \] \[ r_2 = a(1 + e) = 2.5 \times 10^8 (1 + 0.20) = 2.5 \times 10^8 \times 1.20 = 3.0 \times 10^8 \text{ km} \] ### Step 6: Use conservation of angular momentum The angular momentum \(L\) at perihelion and aphelion is conserved: \[ L = m \cdot r_1 \cdot v_1 = m \cdot r_2 \cdot v_2 \] where \(v_1\) is the speed at perihelion and \(v_2\) is the speed at aphelion. Since mass \(m\) cancels out: \[ r_1 \cdot v_1 = r_2 \cdot v_2 \] ### Step 7: Solve for speed at aphelion Substituting the known values: \[ (2.0 \times 10^8) \cdot (81) = (3.0 \times 10^8) \cdot v_2 \] \[ 162 \times 10^8 = 3.0 \times 10^8 \cdot v_2 \] \[ v_2 = \frac{162 \times 10^8}{3.0 \times 10^8} = 54 \text{ km/s} \] ### Final Answer The speed of the comet at aphelion is **54 km/s**.

To solve the problem, we need to find the speed of the comet at aphelion given its speed at perihelion and the distance between the perihelion and aphelion. ### Step 1: Understand the terms - **Perihelion (r₁)**: The point in the orbit where the comet is closest to the star. - **Aphelion (r₂)**: The point in the orbit where the comet is farthest from the star. - The distance between perihelion and aphelion is given as \(1.0 \times 10^8\) km. ### Step 2: Relate perihelion and aphelion distances ...
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