HW15 - MAE146: Astronautics Homework Assigned: Friday,...

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MAE146: Astronautics – Homework Assigned: Friday, March 5 th , 2010 Due date: Optional homework This is simply an optional problem to help you think about fy-bys (and design one oF the project) rather than a real homework. Since you need to the design a fy-by For the project, no homework is assigned this week and you should indeed take this time to work on the project! On the analysis of Venus Fy-bys Assume the Earth to be in a circular orbit around the Sun (with a radius R E ) and a spacecraft in a circular orbit around the Earth (with radius r s ) and let us consider an impulsive maneuver performed along the velocity vector of the spacecraft (as measured relative to a planet centered inertial frame at the time of the maneuver) resulting in an escaping trajectory (from the Earth). 1. On departing angle: (a) Compute the maximum speed of the spacecraft relative to the Sun just after leaving the Earth in±uence. What is the angle between Δ V and the velocity of the Earth relative to the Sun, v V E at the time of the maneuver? Plot a few orbit (in the planet centric frame) with di²erent Δ
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This note was uploaded on 03/13/2010 for the course MAE 19100 taught by Professor Villac during the Winter '10 term at UC Irvine.

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