Mathematical Problems in Engineering / 2015 / Article / Fig 5

Research Article

Lunar CubeSat Impact Trajectory Characteristics as a Function of Its Release Conditions

Figure 5

CubeSat impact parameter characteristics during the impact phase. (a) CubeSat flight time, (b) cross range distance, (c) impact angle, and (d) impact velocity.
(a)
(b)
(c)
(d)

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