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


AIAAPERFORMANCE OF THE TERMINATOR TETHERª FOR AUTONOMOUS DEORBIT OF LEO SPACECRAFT R. Hoyt and R. Forward Tethers Unlimited, Inc., Seattle, WA
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Document Date: 2011-04-12 17:38:09


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File Size: 400,99 KB

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City

Seattle / Nordheim / /

Company

Tethers Unlimited Inc. / R. Forward Tethers Unlimited Inc. / Robert L. Forward Tethers Unlimited Inc. / /

Facility

American Institute of Aeronautics / A Power System / RF Receiver Current Power System / /

IndustryTerm

constellation satellite / cross product / orbital energy / tether device electronics / satellite deorbit / tether systems / drag enhancement devices / tether device / satellite disposal options / electronics / bare metal / typical satellite / area-time product / satellite surface / feedback control algorithm / electron emission device / polar satellite / control electronics / host spacecraftÕs power systems / host satellite / satellite system / areatime product / data acquisition electronics / /

Organization

American Institute of Aeronautics and Astronautics / US Federal Reserve / Tether Control Unit / Magnetic Field Gravity Gradient Force / National Aeronautics and Space Administration / eConducting Hoytether™ Current Drag Force Terminator Tether™ Deployer / Electronics / and Electron Emitter Earth's Magnetic Field Gravity Gradient Force / /

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Position

Vp / Chief Scientist / conductor / Vice President / Chief Engineer / Vp Electrical Characteristics / President / CEO / /

Product

TetherSim / /

ProgrammingLanguage

DC / /

ProvinceOrState

Washington / /

Technology

4th order Runge-Kutte algorithm / radiation / Terminator Tetherª technology / a Field Emission Array / simulation / feedback control algorithm / /

SocialTag