Spacecraft and Aircraft Dynamics - Lecture 5 - Illinois Institute of ...
Spacecraft and Aircraft Dynamics - Lecture 5 - Illinois Institute of ...
Spacecraft and Aircraft Dynamics - Lecture 5 - Illinois Institute of ...
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Example: Jupiter FlybyProblem: Suppose we want to make a flyby <strong>of</strong> Jupiter. The relative velocity atapproach is v ∞ = 10km/s. To achieve the proper turning angle, we need aneccentricity <strong>of</strong> e = 1.07. Radiation limits our time within radius r = 100,000kmto 1 hour (radius <strong>of</strong> Jupiter is 71,000km). Will the spacecraft survive the flyby?M. Peet <strong>Lecture</strong> 5: <strong>Spacecraft</strong> <strong>Dynamics</strong> 15 / 26
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