Plasma accelerator system
First Claim
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1. A METHOD OF PRODUCING PLASMA PROPULSION FOR SPACECRAFT ATTITUDE CONTROL OR THE LIKE, COMPRISING PRODUCING A RADIAL ELECTRIC FIELD WITH AN EVACUATED GAP BETWEEN CONCENTRIC ELECTRODES, PRODUCING A MAGNETIC FIELD AXIALLY OF SAID GAP, SAID MAGNETIC FIELD DIVERGING THROUGHOUT THE AXIAL LENGTH OF THE ELECTRODES, PERIODICALLY INTRODUCING PULSES OF LOW-DENSITY GAS INTO SAID GAP, AND CAUSING A CURRENT TO PASS BETWEEN SAID ELECTRODES IN TIMED RELATION WITH INTRODUCTION OF SAID GAS PULSES TO CREATE A FLOW OF
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1 Claim
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1. A METHOD OF PRODUCING PLASMA PROPULSION FOR SPACECRAFT ATTITUDE CONTROL OR THE LIKE, COMPRISING PRODUCING A RADIAL ELECTRIC FIELD WITH AN EVACUATED GAP BETWEEN CONCENTRIC ELECTRODES, PRODUCING A MAGNETIC FIELD AXIALLY OF SAID GAP, SAID MAGNETIC FIELD DIVERGING THROUGHOUT THE AXIAL LENGTH OF THE ELECTRODES, PERIODICALLY INTRODUCING PULSES OF LOW-DENSITY GAS INTO SAID GAP, AND CAUSING A CURRENT TO PASS BETWEEN SAID ELECTRODES IN TIMED RELATION WITH INTRODUCTION OF SAID GAS PULSES TO CREATE A FLOW OF
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Current AssigneeBernard Gorowitz, Kenneth G. Moses, Per Gloersen
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Original AssigneeBernard Gorowitz, Kenneth G. Moses, Per Gloersen
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InventorsPER GLOERSEN, BERNARD GOROWITZ, Moses, Kenneth G.
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Application NumberUS03/834,574Time in Patent Office1,869 DaysField of SearchUS Class Current310/11CPC Class CodesF03H 1/00 Using plasma to produce a r...F42B 10/663 using a plurality of transv...H05H 1/54 Plasma accelerators
