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Materials science / Spacecraft design / Gyroscopes / Actuators / Microelectromechanical systems / Transducers / Control moment gyroscope / Attitude control / Comb drive / Spaceflight / Technology / Microtechnology


MEMS Control Moment Gyroscope Design and Wafer-Based Spacecraft Chassis Study a a
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Document Date: 2003-07-05 01:33:00


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File Size: 140,86 KB

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City

Seattle / Washington / Pasadena / Wafer / /

Company

Jet Propulsion Laboratory / Applications 12th IEEE International Micro Electro Mechanical Systems / /

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Facility

University of Washington / NASA Institute / /

IndustryTerm

pico-satellite / metal / power generation systems / large systems / Momentum devices / actual device / rugged device / integrated satellite / multi-chip-module technology / satellite containing / cross product / electrostatic rotary devices / solar electricity / space systems / spacecraft subsystem technology / microspacecraft applications / chemical thrusters share / silicon processing techniques / space applications / aerospace community / satellite teams / satellite attitude control / /

Organization

University of Washington / US Federal Reserve / NASA Institute for Advanced Concepts / /

Person

A. Lipson / Mark Campbell / T. Leitner / E. K. Antonsson / Joel Reiter / T. D. Conto / V / E. Socher / R. B. Cohn / S. W. Janson / D. J. Setter / D. H. Lewis / Jr. / N.Fabre / S. Kaldor / Y. Nemirovsky / /

Position

co-operative / /

Product

Disk Suspension / Plate Suspension / /

ProvinceOrState

Washington / /

Technology

150 m 2 m 3.44 g/cm3 MEMS technologies / Microelectromechanical Systems / optical sensing / MEMS / multi-chip-module technology / actual implementation using MEMS technology / simulation / MEMS spacecraft subsystem technology / /

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