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Space technology / CubeSat / Ion thruster / Hall effect thruster / Field-emission electric propulsion / Satellite / Pulsed plasma thruster / Spacecraft / Spacecraft propulsion / Aerospace engineering


IAC-11-C4.6.5
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Document Date: 2012-04-26 09:14:13


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City

Science / AIAA / Barcelona / Small Satellites / San Sebastian / El Segundo / Reston / Wiesbaden / /

Company

Microcosm Press / Cape Town SA. / Alta SpA / Cathode Technologies / Emerging Technologies / Salvo Marcuccio Alta SpA / Pierpaolo Pergola Alta SpA / Andrea Ruggiero Alta SpA / /

Country

Italy / Japan / United States / Spain / /

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Event

Product Issues / /

Facility

California Polytechnical Institute / Stanford University / Space Technology Library / ELECTRIC PROPULSION OPTIONS FOR CUBESATS Pierpaolo Pergola Alta SpA / California Polytechnic State University / Hall Effect Thrusters / /

IndustryTerm

energy storage subsystem / chemical thrusters / high energy density / nano-satellite applications12 / cold gas thrusters / Classical chemical thrusters / real satellite / power electronics / control electronics / communications subsystem / energy / on-board electronics / stored energy / light devices / electric propulsion technologies / orbital energy causing reentry / electric propulsion devices / onboard energy management / active systems / cold gas thruster / active thermal control devices / on-board available energy / /

Organization

U.S. Securities and Exchange Commission / California Polytechnic State University / Congress / Stanford University / National Aeronautics and Space Administration / /

Person

Ion Thruster / C. Rossi / /

Position

general data handling / representative / T.D. / /

Product

3U / Simplified FEEP21 / materials / /

ProvinceOrState

Virginia / New York / Utah / California / /

SportsLeague

Stanford University / /

Technology

radiation / electric propulsion technologies / ESA / EP technologies / MEMS / ISP / simulation / flash / three technologies / /

URL

http /

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