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A method for generating a discharge plasma which covers a surface of a body in a gas at pressures from 0.01 Torr to atmospheric pressure, by applying a radio frequency power with frequencies between approximately 1 MHz and 10 GHz across a plurality of paired insulated conductors on the surface. At t

A method for generating a discharge plasma which covers a surface of a body in a gas at pressures from 0.01 Torr to atmospheric pressure, by applying a radio frequency power with frequencies between approximately 1 MHz and 10 GHz across a plurality of paired insulated conductors on the surface. At these frequencies, an arc-less, non-filamentary plasma can be generated to affect the drag characteristics of vehicles moving through the gas. The plasma can also be used as a source in plasma reactors for chemical reaction operations.

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1. A method for generating a discharge plasma which covers a surface of a body in a gas, comprising: disposing adjacent to a surface of a body in a gas a plurality of paired insulated conductors, said paired insulated conductors forming an array of twin-lead transmission lines, wherein one lead o

1. A method for generating a discharge plasma which covers a surface of a body in a gas, comprising: disposing adjacent to a surface of a body in a gas a plurality of paired insulated conductors, said paired insulated conductors forming an array of twin-lead transmission lines, wherein one lead of said twin-lead transmission lines serves as a first electrode terminal and the remaining lead of said twin-lead transmission lines serves as a second electrode terminal; connecting said first electrode terminal to a first pole of a radio frequency power source which has first and second opposite poles, and connecting the second electrode terminal either to the second pole of said radio frequency power source or to a ground; and generating a discharge plasma which covers the surface of said body utilizing said radio frequency power source to energize said first electrode terminal relative to said second electrode terminal with a radio frequency driving voltage at a frequency greater than approximately 1 MHz. 2. The method of claim 1 wherein said frequency is greater than approximately 10 MHz. 3. The method of claim 1 wherein said frequency is less than approximately 10 GHz. 4. The method of claim 1 wherein said gas is selected from the group comprising air, helium, neon, argon, chlorine, hydrogen bromide, silane, carbon tetraflouride, NF3,boron trichloride, Freon, sulphur hexaflouride, hydrogen, deuterium, nitrogen, ammonia, germane, dichlorosilane, nitrous oxide, C2F6,C4F8,tetraethosiloxane, oxygen, fluorine, carbon monoxide, carbon dioxide, water, hydrogen fluoride, and hydrogen chloride. 5. The method of claim 1 wherein said gas is at a pressure greater than approximately 0.008 Torr. 6. The method of claim 5 wherein said gas is at a pressure of less than approximately 800 Torr. 7. The method of claim 1 wherein said body is a vehicle. 8. The method of claim 1 wherein the discharge plasma which covers the surface of said body reduces the drag of said body in said gas. 9. The method of claim 7 wherein said vehicle is an aircraft. 10. The method of claim 7 wherein said discharge plasma is arc-less and non-filamentary. 11. The method of claim 1 wherein said array of twin-lead transmission lines is arranged in a cylindrical geometry. 12. The method of claim 1 wherein said array of twin-lead transmission lines is arranged in a serpentine winding geometry. 13. The method of claim 1 wherein said array of twin-lead transmission lines is disposed on a printed circuit board. 14. The method of claim 1 wherein said surface is flat. 15. The method of claim 1 wherein said surface is curved. 16. The method of claim 1 wherein said radio frequency power source is applied as a traveling wave. 17. The method of claim 1 wherein said radio frequency power source is applied to opposite ends of said array of twin-lead transmission lines. 18. The method of claim 1 wherein said radio frequency power source driving voltage and frequency is varied, thereby varying the intensity of the generated discharge plasma and varying the drag coefficient of said body. 19. The method of claim 1 wherein the discharge plasma is utilized in a plasma reactor. 20. The method of claim 1 wherein the discharge plasma is applied to surface regions of a jet engine, thereby modifying the airflow to improve propulsion performance.