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Home › System and method for adjusting the orbit of an orbiting space object using an electrodynamic tether and micro-fabricated field emission device

System and method for adjusting the orbit of an orbiting space object using an electrodynamic tether and micro-fabricated field emission device

US Patent 6459206 · Granted Oct 1, 2002

Estimated economic value: $2,679,000 ⓘ

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