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Spacecraft propulsion / Astrodynamics / Space colonization / Space access / Rocket-powered aircraft / Mass driver / Rocket / Escape velocity / Specific impulse / Space technology / Aerospace engineering / Transport


Document Date: 2008-01-02 12:31:08

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City

Philadelphia / Cambridge / /

Company

Sudbury / Cox / MIT Press / Apollo / Amor / /

Currency

pence / /

Facility

Jerome Pearson** U. S. Air Force Flight Dynamics Laboratory Wright-Patterson Air Force Base / Technical University of Munich / /

IndustryTerm

solar 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 / /

Organization

African Union / MIT / US Federal Reserve / Technical University of Munich / National Aeronautics and Space Administration / /

Person

Harry / Ross / Bender / Jerome Pearson / /

Position

author / 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 / /

Product

ROTARY ROCKET / /

ProvinceOrState

Ohio / Ontario / /

PublishedMedium

Scientific American / /

Technology

ISP / /

SocialTag