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A CSC of 16800 kg mass with electrodynamic tether system (EDTS). SBs are not displayed.
The upper circular orbit (300 km altitude)-- 7730 m/s.
Reduction of the CSC speed in the upper circular orbit in course of capturing of the first portion of cargo of 50 kg mass is 23 m/s.
Reduction of the CSC speed in perigee of the elliptical orbit in course of capturing of the second portion of cargo of 50 kg mass is 23 m/s.
The lower circular orbit (220 km altitude) -- 7777 m/s.
Electric power of the membrane SB -- 2.5 MW
FC electric power -- 1 MW.
EDTS electric power -- 1 MW.
FC charging efficiency -- 0.6
SB mass -- 1250 kg (0.5 kg/KW)
FC mass -- 1000 kg (1 kg/KW)
EDTS mass -- 5000 kg
Cargoes' catcher mass -- 1000 kg.
The rest equipment mass -- 8550 kg.
Mass of the captured portion of cargo -- 50 kg.
Length of the track of the cargo substance -- 8000 m.
Time of track capturing -- 1 s.
Acceleration of braking in course of cargo capturing -- 23 m/s2 (~2.3g)
Number of operations on cargo capturing in points 1 and 2 for 1 year -- 8000.
Mass of the captured cargo for 1 year -- 400 tons.
Mass of the cargo used in correction ERE for 1 year -- 0.1-1 tons.
Mass of the cargo accumulated in the orbit for 1 year -- 400 tons.
The fleet of multiuse suborbital rockets for exploitation in course of 1 year -- 20-40 pieces (with 200-400 launches/rocket endurance).

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