U.S. patents available from 1976 to present.
U.S. patent applications available from 2005 to present.

Electromagnetic transportation system for manned space travel

Patent 4795113 Issued on January 3, 1989. Estimated Expiration Date: Icon_subject October 14, 2006. Estimated Expiration Date is calculated based on simple USPTO term provisions. It does not account for terminal disclaimers, term adjustments, failure to pay maintenance fees, or other factors which might affect the term of a patent.

Patent References

3224375

3231219

3325123

3392941

3566800

3596604

Nonbursting magnetic liquid seals for high vacuum applications Patent #: 4445696
Issued on: 05/01/1984
Inventor: Raj ,   et al.

Inventor

Application

No. 06/919252 filed on 10/14/1986

US Classes:

244/63, Launching104/138.1, TUBULAR WAY104/282, Propulsion means employed to suspend car104/292, Propulsion by active guideway; e.g., linear synchronous motor, etc.244/171.3, Launch from surface to orbit335/219Combined with diverse-type art device

Examiners

Primary: Barefoot, Galen L.

Attorney, Agent or Firm

International Classes

B64G 1/14 (20060101)
B64G 1/00 (20060101)
B64G 5/00 (20060101)

Abstract

An electromagnetically propelled space transportation system is provided for transporting passengers and/or freight between the Earth's surface and orbiting spaceports via reusable spaceplanes. Each spaceplane is equipped with a plurality of superconducting propulsion coils extending along its fuselage and is accelerated to orbital velocities inside a vacuum tube by a 1,530 km long electromagnetic linear accelerator. The vacuum tube is evacuated by utilizing the accelerator as a giant vacuum pump wherein a free-moving, magnetically propelled, air-tight piston is driven through the entire tube at low speed thereby forcing the air directly out the end. The spaceplanes are equipped with movable wings and other aerodynamic surfaces that are retracted during launching and extended during landing. The accelerator is capable of launching spaceplanes directly to geosynchronous orbits or onto interplanetary trajectories. The accelerator is embedded deep underground with a maximum depth of 46 km and emerges near the summit of a high mountain. The system is powered by the Earth's gravitational field whereby natural hydro and geothermal energy is converted into electrical energy. Since substantially more electrical energy is generated than is used by the accelerator, the system produces vast amounts of clean renewable electrical energy.

Other References

  • Kolm et al., "Electromagnetic Launchers", IEEE Trans. on Magnetics, vol. Mag 16, No. 5, 9-1980
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