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Propulsion / Ion thruster / Helicon Double Layer Thruster / Variable Specific Impulse Magnetoplasma Rocket / Spacecraft propulsion / Aerospace engineering / Space technology


Document Date: 2008-03-11 00:31:14

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File Size: 2,18 MB

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Company

Author Sa / Space Charge Limited / Orbital Sciences / ProLvssorHarold Y. Wachman / /

Currency

USD / Rs / /

Facility

Massachusetts Institute of Technology May / Geosynchronous Spacecraft Prentice Hall / /

IndustryTerm

low density gas / solar cell technology / mobile communications systems / satellite designs / kinetic energy / heavy propulsion systems / satellite runs / atmospheric gas / Propulsion systems / communications mission / ambient gas thruster / ion propulsion systems / gas impinging ion / satellite coverage / ambient gas / thruster technology / electron energy / geosynchronous satellite / energy / utilizing the atmospheric gas / /

Organization

Massachusetts Institute of Technology / Department of Aeronautics and Astronautics / /

Person

Ray Conley Submitted / Jack L.Kerrebrock Thesis Supervisor Accepted / Ray Conley / LEO SATEI / ION THRUSTER / Departmental Graduate / /

Position

author / driver / Supervisor / Chairman / Professor / /

ProvinceOrState

Massachusetts / /

Technology

thruster technology / solar cell technology / ISP / /

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