Research Article
Lunar CubeSat Impact Trajectory Characteristics as a Function of Its Release Conditions
Figure 9
Relative motion between the mother-ship and CubeSat during impact phase. In-plane (left) and out-of-plane (right) direction angle variations for Case A ((a) and (b)), Case B ((c) and (d)), and Case C ((e) and (f)).
(a) |
(b) |
(c) |
(d) |
(e) |
(f) |