The Study of the Asymmetric Multiple Encounters Problem and Its Application to Obtain Jupiter Gravity Assisted Maneuvers

Table 3

Swing-by with Δ𝐸>1.148.

𝑒 = 0.9
𝜓𝑜 = −2.5 rad		Angle of approach		Variation of velocity	Variation of energy
𝜓𝑓 = 3.5 rad
𝜓		𝜓𝐴		Δ𝑉	Δ𝐸
rad	Degree	rad	Degree
2.292	131.32193	4.82564	276.48892	1.15561	1.14820
2.293	131.37922	4.82347	276.36436	1.15533	1.14821
2.294	131.43652	4.82130	276.23991	1.15505	1.14821
2.295	131.49381	4.81913	276.11552	1.15478	1.14821
2.296	131.55111	4.81696	275.99125	1.15451	1.14821
2.297	131.60841	4.81479	275.86709	1.15425	1.14820