orbital quiz 3

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7 Terms

1
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Specific angular momentum axis

w

2
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Eccentricity vector

p

3
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Semilatus rectum

q

4
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Period of an orbit depends most directly on

  1. mass of primary

  2. Semi major axis length

5
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For a parabolic orbit escape velocity depends most directly on

  1. Radial distance from central body

  2. Mass of primary

6
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For a hyperbolic orbit the true anomaly of the asymptote depends most directly on

Eccentricity

7
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Information needed to produce Lagrange coefficient

  1. Initial position

  2. Initial velocity