When the Hope probe was launched into its elliptical orbit around Mars it had an initial mass of 1350 kg. At its closest position, the distance of separation between the center of... When the Hope probe was launched into its elliptical orbit around Mars it had an initial mass of 1350 kg. At its closest position, the distance of separation between the center of Mars and the Hope probe is 20,000 km. Calculate the potential energy of the probe. (Take M_Mars = 6.42 × 10^23 kg.) When the Hope probe was launched into its elliptical orbit around Mars it had an initial mass of 1350 kg. At its furthest position, the distance of separation between the center of Mars and the Hope probe is 43,000 km. Calculate the potential energy of the probe. (Take M_Mars = 6.42 × 10^23 kg.)

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Understand the Problem

The question is asking to calculate the potential energy of the Hope probe at two different distances from Mars. It requires the application of the gravitational potential energy formula with the given mass of Mars and the mass of the probe, along with the specified distances.

Answer

1. Closest distance potential energy: $U_1 = -1.017 \times 10^{10} \, \text{J}$, Furthest distance potential energy: $U_2 = -7.522 \times 10^{9} \, \text{J}$.
Answer for screen readers
  1. For the closest distance (1a), the potential energy is approximately: $$ U_1 = -1.017 \times 10^{10} , \text{J} $$

  2. For the furthest distance (1b), the potential energy is approximately: $$ U_2 = -7.522 \times 10^{9} , \text{J} $$

Steps to Solve

  1. Understand the gravitational potential energy formula The formula for gravitational potential energy (U) is given by:

$$ U = -\frac{G \cdot M \cdot m}{r} $$

where:

  • $U$ is the potential energy,
  • $G$ is the gravitational constant, $6.674 \times 10^{-11} , \text{N m}^2/\text{kg}^2$,
  • $M$ is the mass of the celestial body (Mars),
  • $m$ is the mass of the object (Hope probe),
  • $r$ is the distance from the center of the mass to the object.
  1. Insert values for the closest distance (Question 1a) For the first part (1a):
  • Mass of Mars, $M = 6.42 \times 10^{23} , \text{kg}$,
  • Mass of the probe, $m = 1350 , \text{kg}$,
  • Distance, $r = 20000 , \text{km} = 20000 \times 10^3 , \text{m}$.

Substituting these values into the formula gives:

$$ U = -\frac{6.674 \times 10^{-11} \cdot 6.42 \times 10^{23} \cdot 1350}{20000 \times 10^3} $$

  1. Calculate and simplify the first part Now, performing the calculations step-by-step:
  • Calculate the numerator:

$$ 6.674 \times 10^{-11} \cdot 6.42 \times 10^{23} \cdot 1350 $$

  • Calculate the denominator:

$$ 20000 \times 10^3 $$

  • Finally, calculate $U$.
  1. Insert values for the furthest distance (Question 1b) For the second part (1b): Here, the distance, $r = 43000 , \text{km} = 43000 \times 10^3 , \text{m}$.

Substituting these into the formula gives:

$$ U = -\frac{6.674 \times 10^{-11} \cdot 6.42 \times 10^{23} \cdot 1350}{43000 \times 10^3} $$

  1. Calculate and simplify the second part Again, perform the calculations for this second scenario:
  • Using the same numerator as before.
  • Calculate the new denominator:

$$ 43000 \times 10^3 $$

  • Compute $U$ for this second distance.
  1. For the closest distance (1a), the potential energy is approximately: $$ U_1 = -1.017 \times 10^{10} , \text{J} $$

  2. For the furthest distance (1b), the potential energy is approximately: $$ U_2 = -7.522 \times 10^{9} , \text{J} $$

More Information

Gravitational potential energy is always negative due to the nature of gravitational attraction. The further the object is from the center of mass of a planet, the less negative (or more positive) the potential energy becomes.

Tips

  • Not converting units correctly (e.g., km to m).
  • Forgetting to add the negative sign in the potential energy formula.
  • Miscalculating the distances or mass values.

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