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Document Date: 2008-01-02 12:31:08Open Document File Size: 268,48 KBShare Result on FacebookCityPhiladelphia / Cambridge / /CompanySudbury / Cox / MIT Press / Apollo / Amor / /Currencypence / /FacilityJerome Pearson** U. S. Air Force Flight Dynamics Laboratory Wright-Patterson Air Force Base / Technical University of Munich / /IndustryTermsolar power satellite construction / energy optimization / chemical rockets / anchored satellite / crew systems / satellite solar power / lunar anchored satellite / metal tube / minimum specific energy / non-dimensional energy efficiency / satellite solar power stations / metal launch tubes / less energy / mining / cislunar transportation / rotational energy / energy supply / energy vs exhaust velocity / synchronous satellite / liquid-hydrogen/liquid-oxygen chemical rocket / energy / /OrganizationAfrican Union / MIT / US Federal Reserve / Technical University of Munich / National Aeronautics and Space Administration / /PersonHarry / Ross / Bender / Jerome Pearson / /Positionauthor / driver / mass driver / D. J. / linear mass driver / collector / Professor / mass driver for moderate exhaust velocities / Acknowledgment The author / Aerospace Engineer / large catcher / mass catcher / catcher / /ProductROTARY ROCKET / /ProvinceOrStateOhio / Ontario / /PublishedMediumScientific American / /TechnologyISP / /SocialTag |