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

Table 1

List of required divert delta-Vs with respect to arbitrary selected out-of-plane deploy angles.

Out-of-plane deploy angle (deg)	Min. divert delta-V (m/s)	Max. divert delta-V (m/s)
90	More than 90	N/A
100	67.50	90.00
110	51.50	90.00
120	41.00	90.00
130	34.00	90.00
140	29.50	90.00
150	27.00	90.00
160	25.00	90.00
170	24.00	90.00
180	23.50	90.00