GB1521327A - High-frequency plasma drive - Google Patents
High-frequency plasma driveInfo
- Publication number
- GB1521327A GB1521327A GB4594075A GB4594075A GB1521327A GB 1521327 A GB1521327 A GB 1521327A GB 4594075 A GB4594075 A GB 4594075A GB 4594075 A GB4594075 A GB 4594075A GB 1521327 A GB1521327 A GB 1521327A
- Authority
- GB
- United Kingdom
- Prior art keywords
- plasma
- generator
- resonator
- discharge chamber
- magnetic field
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired
Links
Classifications
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01J—ELECTRIC DISCHARGE TUBES OR DISCHARGE LAMPS
- H01J27/00—Ion beam tubes
- H01J27/02—Ion sources; Ion guns
- H01J27/16—Ion sources; Ion guns using high-frequency excitation, e.g. microwave excitation
- H01J27/18—Ion sources; Ion guns using high-frequency excitation, e.g. microwave excitation with an applied axial magnetic field
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
- F03H—PRODUCING A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
- F03H1/00—Using plasma to produce a reactive propulsive thrust
- F03H1/0081—Electromagnetic plasma thrusters
-
- H—ELECTRICITY
- H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
- H05H—PLASMA TECHNIQUE; PRODUCTION OF ACCELERATED ELECTRICALLY-CHARGED PARTICLES OR OF NEUTRONS; PRODUCTION OR ACCELERATION OF NEUTRAL MOLECULAR OR ATOMIC BEAMS
- H05H1/00—Generating plasma; Handling plasma
- H05H1/24—Generating plasma
- H05H1/46—Generating plasma using applied electromagnetic fields, e.g. high frequency or microwave energy
Landscapes
- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Plasma & Fusion (AREA)
- Electromagnetism (AREA)
- Spectroscopy & Molecular Physics (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Plasma Technology (AREA)
Abstract
1521327 Jet propulsion plant MESSERSCHMITT-BÍLKOW-BLOHM GmbH 5 Nov 1975 [16 Nov 1974] 45940/75 Heading F1J [Also in Division H1] A high frequency plasma drive comprises a “ # high frequency generator 7 coaxially coupled to a “ # resonator 8 which forms part of an open ended discharge chamber 11 in which a uniform magnetic field is produced by coil 15 and in which propellant gas is ionized and the plasma subsequently accelerated, wherein the intensity of the magnetic field in the discharge chamber, the frequency of the generator and the density of the plasma are so arranged that the dielectric constant of the plasma is negative whereby Lorentz forces acting on the plasma are subject to resonance-like intensification. As shown, the generator and discharge chamber are formed by coaxial tubes 2, 3 inter-connected by a disc 4, all of silver plated copper, the generator 7 being energized by a planar-triode 5 through an isolating capacitor 6. The cylindrical cavity circuits i in the generator and resonator interconnected through an inductive coupling loop 9. Mercury vapour is introduced through a distributer 12 into the discharge chamber 11 which is closed at one end by a quartz disc 10. When drive is put into operation the gas discharge ignites in the electrical field of the resonator without a special ignition device and the plasma is accelerated from the chamber by Lorentz forces. The mechanism of this acceleration and the factors influencing it are theoretically discussed in some detail. In a modification, Fig. 2 (not shown), a quartz plasma boundary anchor (21) followed by acceleration and retardation electrodes (22) is provided at the open end of the resonator to accelerate the ions, which may be neutralized by electrons from an axially disposed hollow cathode (23). The current density may be varied by means of the intensity of the magnetic field.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19742454458 DE2454458C3 (en) | 1974-11-16 | 1974-11-16 | High frequency plasma engine |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1521327A true GB1521327A (en) | 1978-08-16 |
Family
ID=5931045
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB4594075A Expired GB1521327A (en) | 1974-11-16 | 1975-11-05 | High-frequency plasma drive |
Country Status (2)
Country | Link |
---|---|
DE (1) | DE2454458C3 (en) |
GB (1) | GB1521327A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2229865A (en) * | 1988-11-01 | 1990-10-03 | Roger John Shawyer | Electrical propulsion unit for spacecraft |
GB2334761A (en) * | 1998-04-29 | 1999-09-01 | Roger John Shawyer | Microwave thruster for spacecraft |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2952046C2 (en) * | 1979-12-22 | 1982-04-15 | Deutsche Forschungs- und Versuchsanstalt für Luft- und Raumfahrt e.V., 5300 Bonn | Method and device for generating an electrical discharge in a gas flowing at supersonic speed |
CN114810527B (en) * | 2022-06-28 | 2022-09-09 | 国科大杭州高等研究院 | Gas reverse injection distributor anode integrated structure of low-power Hall thruster |
Family Cites Families (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2219545A1 (en) * | 1972-04-21 | 1973-10-31 | Messerschmitt Boelkow Blohm | ION ENGINE |
-
1974
- 1974-11-16 DE DE19742454458 patent/DE2454458C3/en not_active Expired
-
1975
- 1975-11-05 GB GB4594075A patent/GB1521327A/en not_active Expired
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2229865A (en) * | 1988-11-01 | 1990-10-03 | Roger John Shawyer | Electrical propulsion unit for spacecraft |
GB2229865B (en) * | 1988-11-01 | 1993-05-05 | Roger John Shawyer | Electrical propulsion unit for spacecraft |
GB2334761A (en) * | 1998-04-29 | 1999-09-01 | Roger John Shawyer | Microwave thruster for spacecraft |
GB2334761B (en) * | 1998-04-29 | 2000-04-19 | Roger John Shawyer | Microwave thruster for spacecraft |
Also Published As
Publication number | Publication date |
---|---|
DE2454458B2 (en) | 1981-04-02 |
DE2454458C3 (en) | 1981-12-10 |
DE2454458A1 (en) | 1976-05-20 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PS | Patent sealed | ||
PCNP | Patent ceased through non-payment of renewal fee |