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Spacecraft propulsion / Satellites / Spaceflight / Electrodynamic tether / Electrodynamics / Space tether / Hoytether / Space debris / Robert P. Hoyt / Transport / Spacecraft / Aerospace engineering


Document Date: 2011-04-12 17:38:09

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Company

BT / Tethers Unlimited Inc. / Interagency Group / The times / Chauncey Uphoff Fortune-Eight Aerospace Industries Inc. / International Debris Coordination Working Group / Robert P. Hoyt Tethers Unlimited Inc. / Aeronautics and Astronautics Inc. / /

Country

Italy / France / Japan / Russia / United States / United Kingdom / China / India / /

Facility

NASA Marshall Space Flight Center / American Institute of Aeronautics / /

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IndustryTerm

satellite mass / orbital energy / planned constellation systems / analytical tools / energy loss / satellite constellation / polar satellite / field emission device / control electronics / typical constellation satellite / satellite system / satellite constellations / energy / metal / bare metal surface / electrodynamic applications / kinetic energy / m2 satellite crosssectional area / drag enhancement devices / area-time product / telecommunications constellations / rocket-based deorbit systems / /

NaturalFeature

P= mT / /

OperatingSystem

L3 / /

Organization

American Institute of Aeronautics and Astronautics / TSS-1R mission / ProSEDS mission / US Space Command / National Aeronautics and Space Administration / Department of Defense / ded / /

Person

Chris Rupp / Clinton / Joseph P. Loftus / Ty / /

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Position

L. Forward / metal conductor / tether conductor / General / conductor / alternate candidate / Magnetic Field Electrodynamic Drag Force Tether Current Conducting Hoytether™ Terminator Tether Deployer/ Controller / controller / deployer/controller / /

ProvinceOrState

Maine / Washington / /

Technology

ESA / 3491 APPLICATION OF THE TERMINATOR TETHER™ ELECTRODYNAMIC DRAG TECHNOLOGY / /

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