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


AIAATHE TERMINATOR TETHERª: AUTONOMOUS DEORBIT OF LEO SPACECRAFT FOR SPACE DEBRIS MITIGATION R. Hoyt and R. Forward
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Document Date: 2011-04-12 17:38:10


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File Size: 869,30 KB

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City

Seattle / Nordheim / /

Company

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

Facility

University of Maryland / American Institute of Aeronautics / A Power System / /

IndustryTerm

constellation satellite / cross product / orbital energy / tether device electronics / satellite passes / tether device / electronics / bare metal / satellite surface / feedback control algorithm / electron emission device / control electronics / host spacecraftÕs power systems / host satellite / data acquisition electronics / /

Organization

American Institute of Aeronautics and Astronautics / University of Maryland / US Federal Reserve / Tether Control Unit / /

Person

Mark Lewis / Stuart Bowman / /

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Position

Vp / Chief Scientist / Terminator Tetherª Vp / Professor / conductor / Vice President / Chief Engineer / Vp One / drag and heating model / President / CEO / /

ProgrammingLanguage

DC / /

ProvinceOrState

Maryland / Massachusetts / Washington / /

Technology

4th order Runge-Kutte algorithm / radiation / Terminator Tetherª technology / aero / simulation / a Spindt / feedback control algorithm / /

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