Net kinetic energy differential guidance and propulsion system f

Details Net kinetic energy differential guidance and propulsion system f Net kinetic energy differential guidance and propulsion system f

1992-03-19

1995-01-03

Huppert, Michael S.

Aeronautics and astronautics

Spacecraft

Attitude control

244164, B64G 124, B64G 134

Patent

active

053779363

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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