Effects of Asymmetries on the Dynamics of Motorized Momentum Exchange Tether and Payloads Injection Precision

Table 2

Parameters of the MMET.

Parameters	Value	Unit
Earth’s gravitation constant:	3.9877848 × 10^14	m^3/s^2
Length of propulsion tether : l	10000	m
Mass of chief satellite:	5000	kg
Mass of payload :	1000	kg
The density of tethers:	970	kg/m^3
Cross-section area of tethers:	6.283 × 10^−5	m^2
The radius of chief satellite:	0.5	m
The height of chief satellite:	1.5	m
The radius of payloads:	0.5	m
The height of payloads:	1.5	m
The radius of the tether:	0.00447207	m