Net kinetic energy differential guidance and propulsion system for satellites and space vehicles
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United States of America Patent
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Jan 3, 1995
Grant Date -
N/A
app pub date -
Mar 19, 1992
filing date -
Mar 19, 1992
priority date (Note) -
Expired
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Abstract
Apparatus and methods of Gravity Guidance and Propulsion of Geosynchronous Satellites, other satellites and space vehicles using net kinetic energy PUSH of Gravity of the electromagnetic spectrum particles which continually irradiate the earth from space, based on the Oppositely Charged Twin Monopole (OCTM) Theory of Matter. Specifically Fully Stabilized Geosynchronous Satellites can be made with the same lift-off weight as Spin Stabilized Geosynchronous Satellites by using GG&P Methods and Rules of mass distribution in the satellite.
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