1. Transfer orbit setup 15 points
Design a Hohmann transfer from Earth (a = 1.0000 AU) to Venus (a = 0.7233 AU). Compute the transfer orbit's semimajor axis and its perihelion and aphelion distances.
Problem set for Unit 6.
Design a Hohmann transfer from Earth (a = 1.0000 AU) to Venus (a = 0.7233 AU). Compute the transfer orbit's semimajor axis and its perihelion and aphelion distances.
Compute both required velocity changes (Δv1 leaving Earth's orbit, Δv2 arriving at Venus's orbit) using the vis-viva equation, and compute the total mission Δv.
Compute the one-way transfer time in days, and compare it (as a ratio) to the Earth-Mars transfer time computed in Lab 06, explaining why the Venus transfer is shorter.
Using r_L1 ≈ R(m2/3m1)^(1/3), compute the Sun-Jupiter L1 distance (Jupiter's orbital radius is 5.2044 AU) and compare it (as a ratio) to the Sun-Earth L1 distance from Lecture 12/Lab 06. Explain why the ratio is much larger than the simple ratio of Jupiter's to Earth's orbital radii alone.
Submit a complete derivation with equations, units, labeled quantities, and a short narrative interpretation for each problem. Show every step; a correct final number without a visible derivation receives partial credit at most, and quoting a lecture number without adapting it to this problem's specific inputs receives no credit for that step.
OpenStax Astronomy 2e (local reference copy: references/openstax-astronomy-2e-extracted.txt), Chapter 3.4-3.6.
materials/ASTR310/data/ where referenced above.