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MMLU-Pro / 10074 / Calculate the minimum Δv required to place a satellite already in…

Problem

Answer published by the source. Consult the official source to check your work against its answer.

question

Calculate the minimum Δv\Delta v required to place a satellite already in Earth's heliocentric orbit (assumed circular) into the orbit of Venus (also assumed circular and coplanar with Earth). Consider only the gravitational attraction of the Sun.
Plain-text mathematical notation (without MathML)
Calculate the minimum Δv required to place a satellite already in Earth's heliocentric orbit (assumed circular) into the orbit of Venus (also assumed circular and coplanar with Earth). Consider only the gravitational attraction of the Sun. 
Original LaTeX notation
Calculate the minimum $\Delta v$ required to place a satellite already in Earth's heliocentric orbit (assumed circular) into the orbit of Venus (also assumed circular and coplanar with Earth). Consider only the gravitational attraction of the Sun. 

category

physics

options

  1. 5800 $\mathrm{~m} / \mathrm{s}$
  2. 7100 $\mathrm{~m} / \mathrm{s}$
  3. 5600 $\mathrm{~m} / \mathrm{s}$
  4. 4900 $\mathrm{~m} / \mathrm{s}$
  5. 6500 $\mathrm{~m} / \mathrm{s}$
  6. 4500 $\mathrm{~m} / \mathrm{s}$
  7. 3000 $\mathrm{~m} / \mathrm{s}$
  8. 5275$\mathrm{~m} / \mathrm{s}$
  9. 6000 $\mathrm{~m} / \mathrm{s}$
  10. 3800 $\mathrm{~m} / \mathrm{s}$

src

scibench-class

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Source and history

Official source

initial import