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MAE 4410: Fundamentals of Astrodynamics Quiz #4 Due: February ...

MAE 4410: Fundamentals of Astrodynamics Quiz #4 Due: February ...

MAE 4410: Fundamentals of Astrodynamics Quiz #4 Due: February ...

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<strong>MAE</strong> <strong>4410</strong>: <strong>Fundamentals</strong> <strong>of</strong> <strong>Astrodynamics</strong><strong>Quiz</strong> <strong>#4</strong><strong>Due</strong>: <strong>February</strong> 11 th , 20091. List the four conic sections and their ranges/values <strong>of</strong> eccentricities.2. List the four conic sections and their ranges/values <strong>of</strong> specific orbital mechanical energies (maybe tacked onto previous question table)3. List the four conic sections and their ranges/values <strong>of</strong> semi-major axes. (may be tacked ontoprevious question table)2μμv = − (4.1)r a4. The escape velocity in terms <strong>of</strong> a circular orbital velocity at the same r p is given by: (hint, the visvivaequation is shown above)A. v = 4vesccirB. v = 2vesccirC. vesc = vcir − μ rpD. vesc = π vcirE. v = 2vesccir


5. For which conic sections is the following two equations valid:vμε =− (5.1)2a2μμ= − (5.2)r a6. In an elliptical orbit, the line <strong>of</strong> _________________________ connects the point <strong>of</strong> closestapproach, generically known as _______________________, and the point <strong>of</strong> farthestexcursion, generically known as _________________________.

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