Circular Orbit Target Capture Using Space Tether-Net System

Table 1

Parameters of free deployment capture simulations.

Target type	Time; expenditure (s)	Targets states; (m, m/s)	Release velocity (m/s)
Static	20	[100, 0, 0], [0, 0, 0]	[4.99, 0, −0.09]
		[200, 0, 0], [0, 0, 0]	[9.98, 0, −0.19]
	40	[150, 0, 0], [0, 0, 0]	[3.75, 0, −0.14]
		[300, 0, 0], [0, 0, 0]	[7.49, 0, −0.29]
Floating	20	[100, 0, 0], [0, 0.1, 0.1]	[4.99, 0.10, −0.09]
		[0, 0, 200], [0, 0.1, 0]	[0.20, 0.10, 10.02]
	40	[100, 0, 0], [0, 0.1, 0.1]	[2.49, 0.10, 0.01]