Low-Thrust Trajectory Design Using Finite Fourier Series Approximation of Pseudoequinoctial Elements

Table 8

Capture parameters of the Earth-Moon transfer trajectory.

Transfer time (days)	Capture time (days)	Rev no.	(rad)	(m/s)	(km/s)	(km/s)	Proportion (%)
5	4.336	13	0.874	170.5	7.483	8.552	87.50
5.5	4.779	14	0.930	173.5	7.366	8.299	88.76
6	5.271	15	1.049	175.5	7.306	8.087	90.34
6.5	5.779	16	1.142	177.1	7.265	7.932	91.59
7	6.256	18	1.205	180.1	7.275	7.857	92.59
7.5	6.760	19	1.265	180.0	7.203	7.702	93.52
8	7.267	20	1.331	180.9	7.215	7.628	94.59
8.5	7.766	21	1.356	181.0	7.131	7.503	95.04