Method of and apparatus for deriving a high pressure, high temperature plasma jet with a dielectric capillary

Apparatus for accelerating a projectile comprising means for deriving a high temperature, high pressure, supersonic plasma jet, said means including:

• a structure having a capillary passage having a longitudinal axis and an elongated wall having an interior wall surface defining a boundary of the passage, an ablatable dielectric ionizable substance being at and directly behind the wall surface, first and second electrodes at spaced locations along the length of the wall, high voltage power supply means for applying a discharge voltage to the first and second electrodes to form a capillary discharge between the electrodes, the dielectric substance including at least one atomic element that is ionized to form a plasma in response to the discharge voltage from the high voltage power supply means being applied between the electrodes, the plasma being formed by the substance imploding radially into the passage from the wall surface in response to the substance being ionized between the electrodes by the discharge voltage from the high voltage power supply means applied between the electrodes, the diametric length across the passage being short relative to the distance between the electrodes, first and second ends of the passage being arranged while the discharge voltage from the high voltage power supply means is applied between the electrodes to respectively enable and prevent the flow of plasma through them, the plasma in the passage forming an electric discharge channel between the electrodes while the discharge voltage from the high voltage power supply means is applied between the electrodes, the capillary passage being configured and the electrodes being positioned so ohmic dissipation occurs in the electric discharge channel in response to the discharge voltage from the high voltage power supply means being applied between the electrodes to produce a high pressure in the passage, the pressure being sufficiently high and the capillary passage being configured to cause the plasma in the passage to flow longitudinally in the passage and through the first end to form the supersonic pulsed plasma jet;
• and means forming an elongated confined bore having an inlet downstream of the first end so that the supersonic pulsed plasma jet flows through the first end into the bore, the pulsed plasma jet flowing into the bore behind the projectile to produce a high pressure gas that acts against the rear of the projectile, the high pressure gas acting on the rear of the projectile having sufficient pressure against the rear of the projectile to accelerate the projectile through a substantial length of the bore.

Apparatus for accelerating a projectile comprising means for deriving a high temperature, high pressure pulsed supersonic plasma jet from a dielectric ionizable substance, said means including:

• a structure having an interior dielectric wall surface forming a capillary passage, high voltage power supply means for applying a discharge voltage between spaced regions along the length of the interior wall surface while the substance extends longitudinally along the wall surface between the regions to form a capillary discharge between the regions, the dielectric substance including at least one atomic element that is ionized to form a plasma in response to the discharge voltage from the high voltage power supply means being applied between the spaced regions, the plasma being formed by the substance radially imploding into the passage from the wall surface in response to the substance being ionized between the spaced regions by the discharge voltage from the high voltage power supply means applied between the spaced regions, the diametric length across the passage being short relative to the distance between the spaced regions, first and second ends of the passage being arranged while the discharge voltage from the high voltage power supply means is applied between the spaced regions to respectively enable and prevent the flow of plasma through them, the plasma in the passage forming an electric discharge channel between the spaced regions while the discharge voltage from the high voltage power supply means is applied between the regions, the capillary passage being configured and the spaced regions being positioned so ohmic dissipation occurs in the electric discharge channel in response to the discharge voltage from the high voltage power supply means being applied between the spaced regions to produce a high pressure in the passage, the pressure being sufficiently high and the capillary passage being configured to cause the plasma in the passage to flow longitudinally in the passage and through the first end to form the pulsed supersonic plasma jet;
• and means forming an elongated confined bore having an inlet downstream of the first end so that the supersonic pulsed plasma jet flows through the first end into the bore, the pulsed plasma jet flowing into the bore behind the projectile to produce a high pressure gas that acts against the rear of the projectile, the high pressure gas acting on the rear of the projectile having sufficient pressure against the rear of the projectile to accelerate the projectile through a substantial length of the bore.

Apparatus for accelerating a projectile comprising means for generating a high temperature, high pressure supersonic pulsed plasma jet, said means including:

• a structure having a capillary passage with an interior dielectric wall surface, the passage having a first open end, a second end and a longitudinal axis, high voltage power supply means for applying a discharge voltage between spaced regions along the length of the interior dielectric wall surface while (a) a dielectric ionizable substance is along the wall surface, (b) the first end of the passage is open and (c) the second, opposite end of the passage is arranged so fluid flow from the passage through it is substantially prevented, the discharge voltage from the high voltage power supply means causing a breakdown along the wall surface, the distance along the longitudinal axis between the spaced regions being great relative to the diametric length of the passage, the breakdown causing the substance along the wall surface to form a plasma that radially implodes into the capillary passage, the ratio of the distance between the spaced regions in the passage and the diametric length of the passage being such that the plasma fills the capillary passage and thence flows out of the first end, the plasma filling the capillary passage forming a capillary electric discharge channel between the spaced regions, the discharge voltage connected to the spaced regions supplying a flow of current from the high voltage power supply means through the plasma in the passage and the ratio of the distance between the spaced regions in the passage and the diametric length of the passage being such as to cause (a) ohmic dissipation in the plasma and transfer of energy to the plasma, (b) a high pressure to be produced in the plasma in response to the ohmic dissipation, the pressure being sufficiently high to cause plasma to flow longitudinally of the passage thence out of the first open end at supersonic speed, and (c) radiation emission and thermal conduction transport of energy from the plasma in the passage to the wall surface to cause the formation of additional plasma that radially implodes and replaces the plasma flowing out of the first end;
• and means forming an elongated confined bore having an inlet downstream of the first end so that the supersonic pulsed plasma jet flows through the first end into the bore, the pulsed plasma jet flowing into the bore behind the projectile to produce a high pressure gas that acts against the rear of the projectile, the high pressure gas acting on the rear of the projectile having sufficient pressure against the rear of the projectile to accelerate the projectile through a substantial length of the bore.

A method of accelerating a projectile through an elongated confined bore comprising the steps of generating a high temperature, high pressure pulsed plasma supersonic jet, the jet being formed by:

• applying a discharge voltage between spaced regions along the length of an interior dielectric wall surface forming a capillary passage having a length between the regions which is great relative to the diametric length of the passage, said discharge voltage being applied while (a) a dielectric ionizable substance is along the wall surface, (b) a first end of the passage is open and (c) a second, opposite end of the passage is arranged so fluid flow from the passage through it is prevented, the discharge voltage causing a breakdown along the wall surface, the breakdown causing the substance along the wall surface to form a plasma that radially implodes into the capillary passage to fill the capillary passage and thence flow out of the first end at supersonic speed, the plasma filing the capillary passage forming a capillary electric discharge channel between the spaced regions, and supplying a flow of current through the plasma in the passage to cause (a) ohmic dissipation in the plasma and transfer of energy from a source of the current flow to the plasma, a high pressure being produced in the plasma in response to the ohmic dissipation, the pressure being sufficiently high to cause plasma to flow longitudinally of the passage and thence out of the first open end at supersonic speed, and (b) radiation emission and thermal conduction transport of energy from the plasma in the passage to the wall surface to cause the formation of additional plasma that radially implodes and replaces the plasma flowing out of the first end;
• and supplying the plasma flowing at supersonic speed through the first end to the bore behind the projectile to produce a high pressure gas that acts against the rear of the projectile, the high pressure gas acting on the rear of the projectile having sufficient pressure against the rear of the projectile to accelerate the projectile through a substantial length of the bore.

Apparatus for accelerating a projectile comprising means for deriving a high temperature, high pressure plasma from a dielectric ionizable substance, said plasma deriving means including a structure having an interior dielectric wall surface forming a capillary passage, high voltage power supply means for applying a discharge voltage between spaced regions along the length of the interior wall surface while the dielectric ionizable substance extends longitudinally along the wall surface completely between the regions to form a capillary discharge between the regions, the dielectric substance including at least one atomic element that is ionized to form a plasma in response to the discharge voltage from the high voltage power supply means being applied between the spaced regions, the plasma being formed in the passage in response to the substance being ionized between the spaced regions by the discharge voltage from the high voltage power supply means applied between the spaced regions, the diametric length across the passage being short relative to the distance between the spaced regions, the plasma in the passage forming an electric discharge channel between the spaced regions while the discharge voltage from the high voltage power supply means is applied to the regions, the capillary passage being configured and the spaced regions being positioned so ohmic dissipation occurs in the electric discharge channel in response to the discharge voltage from the high voltage power supply means being applied between the spaced regions to produce a high pressure in the passage, the pressure being sufficiently high and the capillary passage being configured to cause the plasma in the passage to flow longitudinally in the passage, and means for coupling the plasma into a confined region behind the projectile to produce a high pressure gas that acts against the rear of the projectile, the high pressure gas acting on the rear of the projectile having sufficient pressure against the rear of the projectile to accelerate the projectile through a substantial length of an elongated passage in which the projectile is located.

Apparatus for accelerating a projectile comprising means for deriving a high temperature, high pressure plasma, said means including:

• a structure having a capillary passage having a longitudinal axis and an elongated wall having an interior wall surface defining a boundary of the passage, an ablatable dielectric ionizable substance being at and directly behind the wall surface, first and second electrodes at spaced locations along the length of the wall, high voltage power supply means for applying a discharge voltage to the first and second electrodes to form a capillary discharge between the electrodes, the dielectric substance including at least one atomic element that is ionized to form a plasma in response to the discharge voltage from the high voltage power supply means being applied between the electrodes, the plasma being formed by the substance flowing radially into the passage from the wall surface in response to the substance being ionized between the electrodes by the discharge voltage from the high voltage power supply means applied between the electrodes, the diametric length across the passage being short relative to the distance between the electrodes, the plasma in the passage forming an electric discharge channel between the electrodes while the discharge voltage from the high voltage power supply means is applied between the electrodes, the capillary passage being configured and the electrodes being positioned so ohmic dissipation occurs in the electric discharge channel in response to the discharge voltage from the high voltage power supply means being applied between the electrodes to produce a high pressure in the passage, the pressure being sufficiently high and the capillary passage being configured to cause the plasma in the passage to flow longitudinally in the passage;
• and means for coupling the plasma into a confined region behind the projectile to produce a high pressure gas that acts against the rear of the projectile while the projectile is moving through a passage, the high pressure gas acting on the rear of the projectile having sufficient pressure against the rear of the projectile to accelerate the projectile through a substantial length of the passage through which the projectile is moving.

Apparatus for accelerating a projectile comprising means for deriving a high temperature, high pressure plasma from a dielectric ionizable substance, said means including:

• a structure having an interior dielectric wall surface forming a capillary passage, high voltage power supply means for applying a discharge voltage between spaced regions along the length of the interior wall surface while the substance extends longitudinally along the wall surface between the regions to form a capillary discharge between the region, the dielectric substance including at least one atomic element that is ionized to form a plasma in response to a discharge voltage from the high voltage power supply means being applied between the spaced regions, the plasma being formed by the substance flowing radially into the passage from the wall surface in response to the substance being ionized between the spaced regions by the discharge voltage from the high voltage power supply means applied between the spaced regions, the diametric length across the passage being short relative to the distance between the spaced regions, the plasma in the passage forming an electric discharge channel between the spaced regions while the discharge voltage from the high voltage power supply means is applied between the regions, the capillary passage being configured and the spaced regions being positioned so ohmic dissipation occurs in the electric discharge channel in response to the discharge voltage from the high voltage power supply means being applied between the spaced regions to produce a high pressure in the passage, the pressure being sufficiently high and capillary passage being configured to cause the plasma in the passage to flow longitudinally in the passage;
• and means for coupling the plasma into a confined region behind the projectile to produce a high pressure gas in the confined region that acts against the rear of the projectile, the high pressure gas acting on the rear of the projectile having sufficient pressure against the rear of the projectile to accelerate the projectile through a substantial length of a passage through which the projectile moves.

Apparatus for accelerating a projectile comprising means for generating a high temperature, high pressure plasma, said means including:

• a structure having a capillary passage with an interior dielectric wall surface, the passage having a first end, a second end and a longitudinal axis, high voltage power supply means for applying a discharge voltage between spaced regions along the length of the interior dielectric wall surface while (a) a dielectric ionizable substance is along the wall surface, (b) the first end of the passage is open and (c) fluid flow from the passage through the second end of the passage is substantially prevented, the discharge voltage from the high voltage power supply means causing a breakdown along the wall surface, the distance along the longitudinal axis between the spaced regions being great relative to the diametric length of the passage, the breakdown causing the substance along the wall surface to form a plasma that flows radially into the capillary passage, the ratio of the distance between the spaced regions in the passage and the diametric length of the passage being such that the plasma fills the capillary passage and thence flows out of the first end, the plasma filling the capillary passage forming a capillary electric discharge channel between the spaced regions, the discharge voltage from the high voltage power supply means connected to the spaced regions supplying a flow of current through the plasma in the passage, the ratio of the distance between the spaced regions in the passage and the diametric length of the passage being such as to cause (a) ohmic dissipation in the plasma and transfer of energy to the plasma, (b) a high pressure to be produced in the plasma in response to the ohmic dissipation, the pressure being sufficiently high to cause plasma to flow longitudinally of the passage thence through the first end of the passage, and (c) radiation emission and thermal conduction transport of energy from the plasma in the passage to the wall surface to cause the formation of additional plasma that flows radially and replaces the plasma flowing through the first end;
• and means for coupling the plasma into a confined region behind the projectile to produce a high pressure gas that acts against the rear of the projectile while the projectile is in a passage through which it is accelerated, the high pressure gas acting on the rear of the projectile having sufficient pressure against the rear of the projectile to accelerate the projectile through a substantial length of the passage through which it is accelerated.

A method of accelerating a projectile through a passage in which the projectile is located comprising the steps of generating a high temperature, high pressure plasma, the plasma being formed by:

• applying a discharge voltage between spaced regions along the length of an interior dielectric wall surface forming a capillary passage having a length between the regions which is great relative to the diametric length of the passage, said discharge voltage being applied while (a) a dielectric ionizable substance is along the wall surface, (b) a first end of the capillary passage is open and (c) fluid flow from the capillary passage through a second, opposite end of the passage is prevented, the discharge voltage causing a breakdown along the wall surface, the breakdown causing the substance along the wall surface to form a plasma that flows radially into the capillary passage to fill the capillary passage and thence flows out of the first end, the plasma filling the capillary passage forming a capillary electric discharge channel between the spaced regions, and supplying a flow of current through the plasma is the passage to cause (a) ohmic dissipation in the plasma and transfer of energy from a source of the current flow to the plasma, a high pressure being produced in the plasma in response to the ohmic dissipation, the pressure being sufficiently high to cause plasma to flow longitudinally of the passage and thence out of the first end, and (b) radiation emission and thermal conduction transport of energy from the plasma in the passage to the wall surface to cause the formation of additional plasma that flows radially and replaces the plasma flowing out of the first end;
• and coupling the plasma into a confined region behind the projectile to produce a high pressure gas that acts against the rear of the projectile to accelerate the projectile through the passage in which the projectile is located, the high pressure gas acting on the rear of the projectile having sufficient pressure against the rear of the projectile to accelerate the projectile through a substantial length of the passage in which the projectile is located and through which the projectile moves.

A method of accelerating a projectile through a passage in which the projectile is located comprising the steps of generating a high temperature, high pressure plasma, the ejecting form by applying a discharge voltage between spaced regions along the length of an interior dielectric wall surface forming a capillary passage having a length between the regions which is great relative to the diametric length of the passage, said discharge voltage being applied while (a) a dielectric ionizable substance along the wall surface (b) a first end of the capillary passage is open and (c) fluid flow from a second, opposite end of the capillary passage is prevented, the discharge voltage causing a breakdown along the wall surface, the breakdown causing the substance along the wall surface to form a plasma that radially implodes into the capillary passage to fill the capillary passage, the plasma filling the capillary passage forming a capillary electric discharge channel between the spaced regions, and supplying a flow of current through the plasma in the passage to cause ohmic dissipation in the plasma and transfer of energy from a source of the current flow to the plasma, a high pressure being produced in the plasma in response to the ohmic dissipation, the pressure being sufficiently high and the capillary passage being configured to cause the plasma in the passage to flow longitudinally in the passage;

• and coupling the plasma into a confined region behind the projectile to produce a high pressure gas that acts against the rear of the projectile while it is in the passage through which it travels, the high pressure gas acting on the rear of the projectile having sufficient pressure against the rear of the projectile to accelerate the projectile through a substantial length of the passage through which the projectile is accelerated.