Tether power generator for earth orbiting satellites

Aeronautics and astronautics – Spacecraft – Spacecraft formation – orbit – or interplanetary path

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244167, B64G 120

Patent

active

049231510

ABSTRACT:
A power generation system utilizes an electromagnetic tether having a three conductor, coaxial configuration which allows the circuit to be closed internal to two orbiting objects. An outer cylinder of the tether is a conductor which is used to cut or pass through the earth's magnetic field to produce a voltage output. A cylinder within the outer cylinder is made of a metal such as soft iron and is used to shield a central conductor from the earth's magnetic field. The two outer cylinders are insulated from the center conductor except at one of the tethered objects where they are electrically connected. This causes the end of the center conductor to be at the same electrical potential as the tethered object when there is an infinite load. Useful power is produced at the other object, which may be a space ship, when a switch is closed and the potential is between the outer cylinder and the center conductor.

REFERENCES:
patent: 3363857 (1968-01-01), Vilbig
patent: 3389877 (1968-06-01), Huber et al.
patent: 4097010 (1978-06-01), Colombo et al.
Tethers Open New Space Options, Ivan Bekey, NASA, Astronautics & Aeronaut, Apr. 1983.
Tethers in Space--Birth and Growth of a New Avenue to Space Utilization, by Georg von Tiesenhausen (NASA), Feb. 1984.
Martin Marietta Aerospace Final Study Report: Phase II Study of Selected Tether Applications in Space, Feb. 1985, pp. ii, iii, iv, 16, 18-36.
NAS, Inc., Report Entitled "Forces on an Electrodynamic Tether Power Generator Earth Orbiting Satellite", Jan. 8, 1986.

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