US3201635A - Method and apparatus for producing a plasma - Google Patents

Method and apparatus for producing a plasma Download PDF

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US3201635A
US3201635A US178215A US17821562A US3201635A US 3201635 A US3201635 A US 3201635A US 178215 A US178215 A US 178215A US 17821562 A US17821562 A US 17821562A US 3201635 A US3201635 A US 3201635A
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plasma
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    • HELECTRICITY
    • H05ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
    • H05HPLASMA TECHNIQUE; PRODUCTION OF ACCELERATED ELECTRICALLY-CHARGED PARTICLES OR OF NEUTRONS; PRODUCTION OR ACCELERATION OF NEUTRAL MOLECULAR OR ATOMIC BEAMS
    • H05H1/00Generating plasma; Handling plasma
    • H05H1/24Generating plasma
    • H05H1/26Plasma torches
    • H05H1/32Plasma torches using an arc
    • H05H1/42Plasma torches using an arc with provisions for introducing materials into the plasma, e.g. powder, liquid

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  • This invention relates generally to the production of a plasma, and more particularly to an apparatus and method for producing a highly conductive plasma, having an electron concentration on the order of electrons per cubic centimeter, and having a homogcnous temperature and pressure distribution.
  • a highly conductive plasma having a homogenous temperature and pressure distribution has many, varied, experimental and practical applications.
  • One important application for such a plasma is its use as the working medium in hypersonic electromagnetic plasma accelerators.
  • Plasma accelerators of this type have a wide range of utility, such as providing a source of high-speed flow for aerodynamic testing, and providing a propulsive system for space vehicles.
  • Another application of such a plasma is in the laboratory simulation of the plasma sheath which is formed around a hypersonic reentry vehicle.
  • Plasma-attenuation experiments are performed on the laboratory produced plasma in which telemetry and microwave signals are transmitted through the plasma to determine the effect of the plasma on the transmitted signal; thereby aiding in the solution of the problem of transmitting radio-frequency signals to and from a high altitude hypersonic vehicle.
  • a plasma, or body of ionized gas may be produced by heating a gaseous material to a temperature whereat the molecules of the gas dissociate into positive ions and negative electrons.
  • a suitable plasma i.e., a plasma having a concentration of electrons on the order of 16 per cubic centimeter
  • electrical arc jet apparatus requires an exorbitant amount of electrical power, in the 10 kilowatt range. Further, operation of such a high powered are has been found to result in excessive electrode erosion, and subsequent contamination of the plasma by the eroded electrode particles.
  • One object of the present invention is to provide a new and improved apparatus for producing a highly conductive plasma having a homogenous temperature and pressure distribution.
  • Another object of this invention is to provide a novel method of producing a plasma having an electron concentration on the order of 10 electrons per cubic centimeter.
  • a further object of this invention is to provide an Patented Aug. 17, 1%65 efficient and effective method and apparatus for increasing the conductivity of an electrical arc jet.
  • a still further object of this invention is to provide a method and apparatus for increasing the electron concentration of an arc jet Without increasing the electrical power required in operating the arc.
  • an electrical arc jet apparatus for producing a high temperature gaseous jet and combining therewith a means for seeding the produced jet with an easily ionizable material in order to increase the conductivity of the jet.
  • the apparatus comprises a chamber wherein an electrical arc is struck and maintained between a pair of electrodes.
  • a fluid such as compressed gas, is fed through the arc and heated so as to form a high temperature, gaseous jet.
  • the gaseous jet then passes into a settling chamber located adjacent said electrodes wherein the jet is seeded and mixed with the ionizing agent.
  • the ionizing agent is stored in liquid state, and is passed through a vaporizer prior to injection into the settling chamber, wherein it mixes with and is thermally ionized by the high temperature gaseous jet, thereby producing a highly conductive plasma jet.
  • the alkali metals because of their low ionization potential, are preferred materials for use as ionizing agents.
  • a metallic, thin walled, substantially cylindrical chamber 11, in which the plasma is produced, is closed at its forward end by a transverse Wall 12 and terminates in an expansion nozzle 13 at its after end.
  • a negative electrode or cathode 14 is positioned in transverse wall 12 and extends into chamber 11 along the longitudinal axis thereof.
  • the forward cylindrical wall 15 of chamber 11 serves as the positive electrode or anode and concentrically surrounds cathode 14 as shown.
  • Transverse wall 12 may be formed of suitable insulating material so as to insulate the concentric electrodes 14-, 15 from each other.
  • a circuit l6, containing a direct current generator 17, is connected across cathode 14 and anode 15.
  • the circuit 16 includes a variable resistance 13 by which the current flow through circuit 16 may be selectively varied.
  • Circuit 16 also includes therein a solenoidal coil 19 wrapped about cylindrical anode 15 so as to produce an axial magnetic fiel in chamber 11. This magnetic field spins the electrical discharge or arc struck between electrodes l4, at a high speed; thus preventing burnout of the anode l5, raising the energy input into the arc, and more uniformly heating a fluid, such as a compressed gas, passing through the are.
  • a high-pressure fluid source 21 is connected via conduit 23 and control valve 22 to chamber 11 so as to introduce a fluid flow into chamber ll adjacent electrodes 14, 15 and through an electrical arc struck and maintained between electrodes 14, 15.
  • a preferred fluid for utilization in this plasma generating apparatus is gaseous nitrogen, of which the physical properties are to some extent similar to those of air. The gaseous nitrogen having relatively large molecular size may be readily.
  • a potential source 31 in circuit 29 provides the energy for the heating current flow through circuit 29 and tube 27.
  • a piston member 32 is reciprocable in reservoir 24 to force the liquid ionizing agent 25 from reservoir 24 into vaporizing tube 27 upon opening of valve 28.
  • Other means, such as gas pressure, may be used to force the liquid material 25 from reservoir 24; however it has been found that the use of a piston, as shown, best eliminates any pulsations in the flow of theliquid material 25 from the reservoir.
  • the circuit 16 is first energized to provide an electrical discharge or are between electrodes'14, 1 5 in chamber 11; the coil 19 producing an axial magnetic field in chamber 11.'
  • the gas source 21 is then employed to introduce a gas fiow through conduit 23 into chamber 11 adjacent electrodes 14, 15.
  • the gas flow passes through the arc struck and maintained between electrodes 14, 15, producing a high temperature, gaseous jet.
  • This high temperature jet proceeds into after portion 26 of cylindrical chamber 11 wherein it is seeded with the alkali metal ionizing agent 25 and mixed therewith.
  • the liquid alkali metal 25 in reservoir 24 is forcedtherefrom at a predetermined rate by piston 32 and enters the electrically heated vaporizing tube 27 through flow control valve 28.
  • the liquid metal 25 is vaporized during its transit through tube 27 and is then injected into the after portion 26 of chamber 11 to seed and mix with the high temperature gaseous jet.
  • the chamber after portion 26 serves as a settling chamber wherein the injected alkali metal is evenly mixed with and ionized by the gaseous jet, and the plasma jet produced thereby is accorded a homogenous temperature and pressure distribution.
  • the resulting plasma jet then issues from the expansion nozzle 13 into an accelerator, not shown, or a laboratory testing apparatus, not shown.
  • the above described seeding of a high temperature gaseous jet with an alkali metal produces a highly conductive plasma jet, having an electron concentration on the order of electrons per cubic centimeter.
  • An alkali metal is preferred as the seeding material or ionizing agent because ofits low. ionization'potential; the vaporized alkali metal readily dissociating into positive ions and negative electrons when injected or fed into the high temperature, gaseous jet.
  • the 'metal is vaporized prior to being mixed with the gaseous jet'so that the heat available in the jet may be used wholly to ionize the metal, and need not be expended in vaporizing the liquid metal.
  • the preferred alkali metalfor use in the system is cesium, dissociation energy 0.49 electron volt;
  • a /2 inch diameter water-cooled tungsten rod was-used for the cathode l4 and surrounded by a 1 /8 inch diameter water-cooled copper cylinder for the anode 15.
  • the circuit 16 for striking an are between electrodes 14-, was operated at a voltage of 110' volts and 1,400 amps, or approximately 150 kilowatts.
  • the efiiciency of the are as determined by calorimetric tests was 32 percent, which gives 1 and molecular nitrogen.
  • the reservoir. 24 contained liquid cesium and was formed of Plexiglas. Piston 32 was motor-driven to force the cesium from the reservoir at a flow rate set to give a 2 percent mole-fraction ratio between the cesium V
  • the cesium was vaporized in a A; inch stainless-steel tube inches long, electrically heated to 800 C. With the reservoir 24 containing 10 grams of cesium, the duration of cesium flow was 40 seconds.
  • An apparatus for producing a highly conductive plasma jet comprising: means for striking and maintaina ing an electrical are; means for conveying a fluid to said electrical arc, thereby producing a high temperature,
  • An apparatus for producing a highly conductive plasma jet comprising: means defining a substantially cylindrical chamber having a forward and an after end; means operatively connected thereto for striking and maintaining an electrical arc across the forward end of said chamber; means for conveying a fluid to said electrical are, thereby producing a high temperature, gaseous jet; a reservoir containing a material having a low ionization potential; and means to convey the ionizing materialfrom, said reservoir to the after portion of said chamber to intermingle with and seed the high temperature, gaseous jet passing therethrough, thereby increasing the conductivity of the jet.
  • FOREIGN PATENTS means to convey comprises a vaporizing tube connected 279 825 8/28 Gmat England between said reservoir and the after portion of said chamher, and means for forcing the ionizing material from OTHER REFERENCES said reservoir through said tube and into the after pOr- 5 H d et 1 NAsA Technical N t D480 M 17 tion of said chamber. 1950,

Description

Aug. 17, 1965 A. F. CARTER 3,201,635
METHOD AND APPARATUS FOR PRODUCING A PLASMA Filed March 7, 1962 INVENTOR ARLE/V F.' CARTER BY A ATTO EYS United Sttes atct 3,201,635 Mariano AND arrana'rris son rnonucuso A PLASMA Arlen F. Carter, Newport News, Va, assignor to the United ates of America as represented by the Administrator of the National Aeronautics and dpacc Administration Filed Mar. 7, 1962, Ser. No. 178,215 3 (Ilaians. (Cl. 3l3--l.56) (Granted under Title 35, US. Code (1952), sec. 266) The invention described herein may be manufactured and used by and for the Government of the United States of America for governmental purposes without the payment of any royalties thereon or therefor.
This invention relates generally to the production of a plasma, and more particularly to an apparatus and method for producing a highly conductive plasma, having an electron concentration on the order of electrons per cubic centimeter, and having a homogcnous temperature and pressure distribution.
A highly conductive plasma having a homogenous temperature and pressure distribution has many, varied, experimental and practical applications. One important application for such a plasma is its use as the working medium in hypersonic electromagnetic plasma accelerators. Plasma accelerators of this type have a wide range of utility, such as providing a source of high-speed flow for aerodynamic testing, and providing a propulsive system for space vehicles. Another application of such a plasma is in the laboratory simulation of the plasma sheath which is formed around a hypersonic reentry vehicle. Plasma-attenuation experiments are performed on the laboratory produced plasma in which telemetry and microwave signals are transmitted through the plasma to determine the effect of the plasma on the transmitted signal; thereby aiding in the solution of the problem of transmitting radio-frequency signals to and from a high altitude hypersonic vehicle.
It is well known that a plasma, or body of ionized gas, may be produced by heating a gaseous material to a temperature whereat the molecules of the gas dissociate into positive ions and negative electrons. However, the high degree of ionization required by present day applications has heretofore not been attainable through chemical processes; and the production of a suitable plasma, i.e., a plasma having a concentration of electrons on the order of 16 per cubic centimeter, through use of known electrical arc jet apparatus requires an exorbitant amount of electrical power, in the 10 kilowatt range. Further, operation of such a high powered are has been found to result in excessive electrode erosion, and subsequent contamination of the plasma by the eroded electrode particles.
One object of the present invention is to provide a new and improved apparatus for producing a highly conductive plasma having a homogenous temperature and pressure distribution.
Another object of this invention is to provide a novel method of producing a plasma having an electron concentration on the order of 10 electrons per cubic centimeter.
A further object of this invention is to provide an Patented Aug. 17, 1%65 efficient and effective method and apparatus for increasing the conductivity of an electrical arc jet.
A still further object of this invention is to provide a method and apparatus for increasing the electron concentration of an arc jet Without increasing the electrical power required in operating the arc.
According to the present invention, the foregoing and other objects are attained by providing an electrical arc jet apparatus for producing a high temperature gaseous jet and combining therewith a means for seeding the produced jet with an easily ionizable material in order to increase the conductivity of the jet. The apparatus comprises a chamber wherein an electrical arc is struck and maintained between a pair of electrodes. A fluid, such as compressed gas, is fed through the arc and heated so as to form a high temperature, gaseous jet. The gaseous jet then passes into a settling chamber located adjacent said electrodes wherein the jet is seeded and mixed with the ionizing agent. The ionizing agent is stored in liquid state, and is passed through a vaporizer prior to injection into the settling chamber, wherein it mixes with and is thermally ionized by the high temperature gaseous jet, thereby producing a highly conductive plasma jet. The alkali metals, because of their low ionization potential, are preferred materials for use as ionizing agents.
Other objects and many of the attendant advantages of this invention Will be readily appreciated as the same becomes better understood by reference to the following detailed description when considered in conjunction with the solitary figure of the accompanying drawing wherein is shown a diagrammatic view, partially in section, of the apparatus of the present invention.
Referring now to the drawing, a metallic, thin walled, substantially cylindrical chamber 11, in which the plasma is produced, is closed at its forward end by a transverse Wall 12 and terminates in an expansion nozzle 13 at its after end. A negative electrode or cathode 14 is positioned in transverse wall 12 and extends into chamber 11 along the longitudinal axis thereof. The forward cylindrical wall 15 of chamber 11 serves as the positive electrode or anode and concentrically surrounds cathode 14 as shown. Transverse wall 12 may be formed of suitable insulating material so as to insulate the concentric electrodes 14-, 15 from each other. A circuit l6, containing a direct current generator 17, is connected across cathode 14 and anode 15. The circuit 16 includes a variable resistance 13 by which the current flow through circuit 16 may be selectively varied. Circuit 16 also includes therein a solenoidal coil 19 wrapped about cylindrical anode 15 so as to produce an axial magnetic fiel in chamber 11. This magnetic field spins the electrical discharge or arc struck between electrodes l4, at a high speed; thus preventing burnout of the anode l5, raising the energy input into the arc, and more uniformly heating a fluid, such as a compressed gas, passing through the are.
A high-pressure fluid source 21 is connected via conduit 23 and control valve 22 to chamber 11 so as to introduce a fluid flow into chamber ll adjacent electrodes 14, 15 and through an electrical arc struck and maintained between electrodes 14, 15. A preferred fluid for utilization in this plasma generating apparatus is gaseous nitrogen, of which the physical properties are to some extent similar to those of air. The gaseous nitrogen having relatively large molecular size may be readily.
raised to high temperatures by an electrical arc. Also, the stability of nitrogen at high temperatures limits the likelihood of the high temperature, gaseous, nitrogen combining with the seeded alkali metals, as is discussed subsequently, thus enabling full use to be made of the its own resistance to current passing through circuit 29 connected between chamber portion 26 and tube 27; A potential source 31 in circuit 29 provides the energy for the heating current flow through circuit 29 and tube 27. A piston member 32 is reciprocable in reservoir 24 to force the liquid ionizing agent 25 from reservoir 24 into vaporizing tube 27 upon opening of valve 28. Other means, such as gas pressure, may be used to force the liquid material 25 from reservoir 24; however it has been found that the use of a piston, as shown, best eliminates any pulsations in the flow of theliquid material 25 from the reservoir.
The method of the invention maybest bedescribed with reference to the apparatus shown in the drawing, although it is to be understood that the method may be performed with other apparatus as well.
The circuit 16 is first energized to provide an electrical discharge or are between electrodes'14, 1 5 in chamber 11; the coil 19 producing an axial magnetic field in chamber 11.' The gas source 21 is then employed to introduce a gas fiow through conduit 23 into chamber 11 adjacent electrodes 14, 15. The gas flow passes through the arc struck and maintained between electrodes 14, 15, producing a high temperature, gaseous jet. This high temperature jet proceeds into after portion 26 of cylindrical chamber 11 wherein it is seeded with the alkali metal ionizing agent 25 and mixed therewith. The liquid alkali metal 25 in reservoir 24 is forcedtherefrom at a predetermined rate by piston 32 and enters the electrically heated vaporizing tube 27 through flow control valve 28. The liquid metal 25 is vaporized during its transit through tube 27 and is then injected into the after portion 26 of chamber 11 to seed and mix with the high temperature gaseous jet. The chamber after portion 26 serves as a settling chamber wherein the injected alkali metal is evenly mixed with and ionized by the gaseous jet, and the plasma jet produced thereby is accorded a homogenous temperature and pressure distribution. The resulting plasma jet then issues from the expansion nozzle 13 into an accelerator, not shown, or a laboratory testing apparatus, not shown.
The above described seeding of a high temperature gaseous jet with an alkali metal produces a highly conductive plasma jet, having an electron concentration on the order of electrons per cubic centimeter. An alkali metal is preferred as the seeding material or ionizing agent because ofits low. ionization'potential; the vaporized alkali metal readily dissociating into positive ions and negative electrons when injected or fed into the high temperature, gaseous jet. The 'metal is vaporized prior to being mixed with the gaseous jet'so that the heat available in the jet may be used wholly to ionize the metal, and need not be expended in vaporizing the liquid metal. The preferred alkali metalfor use in the system is cesium, dissociation energy 0.49 electron volt;
however, potassium and sodium have also been favorably employed; An interesting study on the dissociation properties of cesium may be found in National Aero- 1 nautics and'Space Administration Technical Note D-380,
published in May 1960, titled Temperature and Coms,201,ea5 I position 'of a Plasma Obtained by Seeding a Cyanogen- Oxygen Flame with Cesium.
To afford a clearer understanding of the present invention, the physical characteristics of one experimental apparatus constructed and operated in accordance with this invention will now be described. A /2 inch diameter water-cooled tungsten rod was-used for the cathode l4 and surrounded by a 1 /8 inch diameter water-cooled copper cylinder for the anode 15. The circuit 16 for striking an are between electrodes 14-, was operated at a voltage of 110' volts and 1,400 amps, or approximately 150 kilowatts. The efiiciency of the are as determined by calorimetric tests was 32 percent, which gives 1 and molecular nitrogen.
an enthalpy of 8,860 B.t.u./lb. and a stagnation temperature of -6,900 K. The nitrogen from'source 21 was regulated to fiow at 2.6 grams/second. The coil 19 wrapped about anode 15 produced an axial magnetic field of 0.5 Weber/meter? The settling chamber 2 6 was made 2 inches in length, it being found that a greater length resulted in a relatively larger heat loss to the chamber wall. a i
. The reservoir. 24 contained liquid cesium and was formed of Plexiglas. Piston 32 was motor-driven to force the cesium from the reservoir at a flow rate set to give a 2 percent mole-fraction ratio between the cesium V The cesium was vaporized in a A; inch stainless-steel tube inches long, electrically heated to 800 C. With the reservoir 24 containing 10 grams of cesium, the duration of cesium flow was 40 seconds. The resulting plasma emerged from nozzle 13 at a Mach number of approximately 2, a calculated static temperature of 5,500 IQ, and with a cross-sectional area of 1 square centimeter V s It is to be understood that the dimensions given and materials used in the above described exemplary apparatus are merely illustrative of the present invention and that the reduction or enlargement of the physical dimensions of the apparatus, or the substitution of other materials for those described, is well within the scope of the present invention and is contemplated by the inventor thereof. 7 I
Obviously numerous modifications and variations of the present invention are possible in the light of the above teachings. It'is therefore to be understood that within the scope of theappended claims the invention may be practiced otherwise than as described herein.
What is claimed as new and desired to be secured by Letters Patent of the United States is:
1. An apparatus for producing a highly conductive plasma jet comprising: means for striking and maintaina ing an electrical are; means for conveying a fluid to said electrical arc, thereby producing a high temperature,
gaseous jet; a reservoir containing a material having aoutlet for the discharge thereof; conduit means communicating said reservoir with said settling chamber; and means to force said ionizing material fromsaid reservoir through said conduit means into said settling chamber to mix with and seed said jet, thereby increasing the conductivity of the jet.
- 2. An apparatus for producing a highly conductive plasma jet comprising: means defining a substantially cylindrical chamber having a forward and an after end; means operatively connected thereto for striking and maintaining an electrical arc across the forward end of said chamber; means for conveying a fluid to said electrical are, thereby producing a high temperature, gaseous jet; a reservoir containing a material having a low ionization potential; and means to convey the ionizing materialfrom, said reservoir to the after portion of said chamber to intermingle with and seed the high temperature, gaseous jet passing therethrough, thereby increasing the conductivity of the jet.
.5 5 3. An apparatus according to claim 2, wherein said FOREIGN PATENTS means to convey comprises a vaporizing tube connected 279 825 8/28 Gmat Britain between said reservoir and the after portion of said chamher, and means for forcing the ionizing material from OTHER REFERENCES said reservoir through said tube and into the after pOr- 5 H d et 1 NAsA Technical N t D480 M 17 tion of said chamber. 1950,
Rosa: R. 1., Shock Wave Spectroscopy and Engi- Eegerences Cum} by the Examiner neering Magnetohydrodynamics," thesis, Cornell Uni- UNITED STATES PATENTS versity, 1955, pages 30 to 45 relied upon.
3,014,154 12/61 Ehlers et a1 313231.5 X 10 V I 3,029,635 5/62 Feiz 313 231.5 X GLGKGE N. WESTBY, Pumary Examlnei. 3,073,984 1/63 Eschenbach et a1. 313161 X 3,075,065 1/63 Ducatiet a1.

Claims (1)

1. AN APPARATUS FOR PRODUCING A HIGHLY CONDUCTIVE PLASMA JET COMPRISING: MEANS FOR STRIKING AND MAINTAINING AN ELECTRICAL ARC; MEANS FOR CONVEYING A FLUID TO SAID ELECTRICAL ARC, THEREBY PRODUCING A HIGH TEMPERATURE, GASEOUS JET; A RESERVOIR CONTAINING A MATERIAL HAVING A LOW IONIZATION POTENTIAL; A SETTLING CHAMBER POSITIONED ADJACENT SAID FIRST NAMED MEANS AND HAVING AN INLET FOR THE INGRESS OF THE HIGH TEMPERATURE, GASEOUS JET AND AN OUTLET FOR THE DISCHARGE THEREOF; CONDUIT MEANS COMMUNICATING SAID RESERVOIR WITH SAID SETTLING CHAMBER; AND MEANS TO FORCE SAID IONIZING MATERIAL FROM SAID RESERVOIR THROUGH SAID CONDUIT MEANS INTO SAID SETTLING CHAMBER TO MIX WITH AND SEED SAID JET, THEREBY INCREASING THE CONDUCTIVITY OF THE JET.
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Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3355605A (en) * 1963-09-23 1967-11-28 American Radiator & Standard Crossed field plasma device
US3376468A (en) * 1965-10-11 1968-04-02 Northern Natural Gas Method and apparatus for heating gases to high temperatures
US3418445A (en) * 1965-04-07 1968-12-24 Ltv Aerospace Corp Apparatus for supplying high energy gas streams to a wind tunnel
US3678323A (en) * 1970-12-08 1972-07-18 Atomic Energy Commission Hydrogen ion beam generating electrode
US3777208A (en) * 1968-07-05 1973-12-04 Chevron Res Method and apparatus for producing radiation
US5003226A (en) * 1989-11-16 1991-03-26 Avco Research Laboratories Plasma cathode
WO2006137205A1 (en) 2005-06-22 2006-12-28 Tokyo Institute Of Technology Liquid introducing plasma system
US8541910B1 (en) * 2003-03-20 2013-09-24 University Of South Florida MEMS microgenerator cell and microgenerator cell array

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB279825A (en) * 1926-10-28 1928-08-02 Ig Farbenindustrie Ag Improvements in heating carbonaceous materials
US3014154A (en) * 1959-10-01 1961-12-19 Kenneth W Ehlers Ion rocket engine
US3029635A (en) * 1956-07-09 1962-04-17 Amalgamated Growth Ind Inc High-temperature testing apparatus
US3073984A (en) * 1961-01-03 1963-01-15 Union Carbide Corp Toroidal arc apparatus
US3075065A (en) * 1960-10-04 1963-01-22 Adriano C Ducati Hyperthermal tunnel apparatus and electrical plasma-jet torch incorporated therein

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB279825A (en) * 1926-10-28 1928-08-02 Ig Farbenindustrie Ag Improvements in heating carbonaceous materials
US3029635A (en) * 1956-07-09 1962-04-17 Amalgamated Growth Ind Inc High-temperature testing apparatus
US3014154A (en) * 1959-10-01 1961-12-19 Kenneth W Ehlers Ion rocket engine
US3075065A (en) * 1960-10-04 1963-01-22 Adriano C Ducati Hyperthermal tunnel apparatus and electrical plasma-jet torch incorporated therein
US3073984A (en) * 1961-01-03 1963-01-15 Union Carbide Corp Toroidal arc apparatus

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3355605A (en) * 1963-09-23 1967-11-28 American Radiator & Standard Crossed field plasma device
US3418445A (en) * 1965-04-07 1968-12-24 Ltv Aerospace Corp Apparatus for supplying high energy gas streams to a wind tunnel
US3376468A (en) * 1965-10-11 1968-04-02 Northern Natural Gas Method and apparatus for heating gases to high temperatures
US3777208A (en) * 1968-07-05 1973-12-04 Chevron Res Method and apparatus for producing radiation
US3678323A (en) * 1970-12-08 1972-07-18 Atomic Energy Commission Hydrogen ion beam generating electrode
US5003226A (en) * 1989-11-16 1991-03-26 Avco Research Laboratories Plasma cathode
US8541910B1 (en) * 2003-03-20 2013-09-24 University Of South Florida MEMS microgenerator cell and microgenerator cell array
WO2006137205A1 (en) 2005-06-22 2006-12-28 Tokyo Institute Of Technology Liquid introducing plasma system
EP1895286A1 (en) * 2005-06-22 2008-03-05 Tokyo Institute Of Technology Liquid introducing plasma system
EP1895286A4 (en) * 2005-06-22 2010-02-03 Tokyo Inst Tech Liquid introducing plasma system

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