UTILIZATION OF AN ENHANCED ARTIFICIAL MAGNETOSPHERE FOR SHIELDING AGAINST SPACE ENVIRONMENTAL HAZARDS

• US 20130037656A1
• Filed: 08/08/2012
• Published: 02/14/2013
• Est. Priority Date: 08/10/2011
• Status: Abandoned Application

• Current Assignee: Integral ElectroMagnetronic Technologies LLC
• Original Assignee: Albert Francis Jr. Messano
• Inventors: Messano, Albert Francis Jr.
• Application Number:
  US13/569,340
• Publication Number:
  US 20130037656A1
• Time in Patent Office: Days
• US Class Current: 244/171.7
• CPC Class Codes: B64G 1/226 Special coatings for spacecraft
• CPC Class Codes: B64G 1/543 protecting the crew in manned spacecraft
• CPC Class Codes: B64G 1/546 shielding electronic equipment
• CPC Class Codes: G21F 3/00 Shielding characterised by its physical form, e.g. granules, or shape of the material
• CPC Class Codes: G21F 7/00 Shielded cells or rooms

Abstract

This invention relates to technology used for creating an enhanced artificial magnetosphere or electromagnetic shield for use in both manned and unmanned spacecraft. The invention includes an Interference Generating Pattern (IGP) which is tuned to the high-frequency radiation of X-rays and gamma rays and a conformal magnetic field. This technology will reduce the exposure of astronauts or other space travelers, as well as radiation-sensitive equipment, to the environmental hazards present therein. The net result will be reduced radiation intensity in order to create a space radiation-free environment as to render space travel safe.

Claims

1. A method of providing a spacecraft with an enhanced artificial magnetosphere or electromagnetic shield, which comprises providing the spacecraft with an Interference Generating Pattern (IGP) which is tuned to high-frequency radiation of X-rays and gamma rays, and embedding electrical current conductors in or near an outer surface of the spacecraft, thus creating an artificial Magnetosphere (AMS) to shield against dangers due to a variety of energetic particles prevalent in outer space.

2. The method of claim 1, wherein the IGP is configured to attenuate high frequency radiation in the range of 10¹³ to 10²⁰ MHZ and to reduce high frequency signals by at least 20 dB to 50 dB.

3. The method of claim 2, wherein the diffraction grating is provided as a paint or coating on one or more of the interior wall(s), ceiling or floor of the spacecraft.

4. The method of claim 1, wherein the IGP is comprised of different patterns constructed with different physical dimensions for each pattern.

5. The method of claim 4, wherein the IGP is comprised of horizontal or vertical layering of the different multiple patterns.

6. An electromagnetic radiation-free spacecraft provided by the method of claim 1.

7. An electromagnetic radiation-free spacecraft that includes a non-conductive interference generating pattern (IGP) which includes a diffraction grating that is tuned to high-frequency radiation of X-rays and gamma rays, and electrical current conductors in or near an outer surface of the spacecraft, thus creating an artificial Magnetosphere (AMS) to shield against dangers due to a variety of energetic particles prevalent in outer space.

8. The spacecraft of claim 7, wherein the IGP is configured to attenuate high frequency radiation in the range of 10¹³ to 10²⁰ MHZ and to reduce high frequency signals by at least 20 dB to 50 dB.

9. The spacecraft of claim 8, wherein the diffraction grating is provided as a paint or coating on one or more of the interior wall(s), ceiling or floor of the spacecraft.

10. The spacecraft of claim 7, wherein the IGP is comprised of different patterns constructed with different physical dimensions for each pattern.

11. The spacecraft of claim 10, wherein the IGP is comprised of horizontal or vertical layering of the different multiple patterns.