Method of and apparatus for accelerating a projectile

• US 4,590,842 A
• Filed: 03/01/1983
• Issued: 05/27/1986
• Est. Priority Date: 03/01/1983
• Status: Expired due to Fees

• Current Assignee: General Dynamics Land Systems Incorporated (General Dynamics Corporation)
• Original Assignee: Gt-devices, Inc.
• Inventors: Tidman, Derek A., Goldstein, Yeshayahu S. A.
• Primary Examiner(s): Brown, David H.
• Assistant Examiner(s): Griffiths, John E.
• Application Number:
  US06/471,215
• Time in Patent Office: 1,183 Days
• Field of Search: 89/8, 89/7, 102/202, 102/291, 124/3, 124/56, 310/10-14, 376/105, 376/108, 376/128, 376/102, 313/231.31, 313/231.41, 313/359.1, 313/360.1, 313/362.1, 315/111.21, 315/111.41, 315/111.61, 315/111.81, 73/12
• US Class Current: 89/8
• CPC Class Codes: F41A 1/02 Hypervelocity missile propulsion using successive means for increasing the propulsive force, e.g. using successively initiated propellant charges arranged along the barrel length; Multistage missile propulsion
• CPC Class Codes: F41B 6/00 Electromagnetic launchers ; Plasma-actuated launchers projectiles for electromagnetic or plasma guns F42B6/006

Abstract

A projectile is accelerated along a confined path by supplying a pulsed high pressure, high velocity plasma jet to the rear of the projectile as the projectile traverses the path. The jet enters the confined path at a non-zero angle relative to the projectile path. The pulse is derived from a dielectric capillary tube having an interior wall from which plasma forming material is ablated in response to a discharge voltage. The projectile can be accelerated in response to the kinetic energy in the plasma jet or in response to a pressure increase of gases in the confined path resulting from the heat added to the gases by the plasma.

Claims

1. Apparatus for accelerating a projectile comprising means forming a confined path having a longitudinal axis along which the projectile traverses, and means for supplying a pulsed high pressure, high velocity plasma jet to the path from outside the path and to the rear of the projectile as the projectile traverses the path to accelerate the projectile along the path, the jet entering the confined path at a non-zero acute angle relative to the confined path axis, the projectile and confined path geometries being such that the plasma to the rear of the projectile has a tendency to leak around the projectile so the leaked plasma is in front of the projectile, the plasma in front of the projectile tending to accumulate and to impede the acceleration of the projectile, and means for venting the plasma in front of the projectile from the confined path to substantially overcome the tendency of the leaked plasma to accumulate and impede the projectile acceleration.

2. The apparatus of claim 1 wherein the means for venting the plasma in front of the projectile from the confined path includes a vacuum chamber surrounding a wall defining the confined path, said chamber having openings into the confined path at several locations around the wall.

3. Apparatus for accelerating a projectile comprising means forming a confined path having a longitudinal axis along which the projectile traverses, and means for supplying a pulsed high pressure, high velocity plasma jet to the path from outside the path and to the rear of the projectile as the projectile traverses the path to accelerate the projectile along the path, the jet entering the confined path at a non-zero acute angle relative to the confined path axis, the means for supplying a pulsed high pressure, high velocity plasma jet to the path including a tube having an interior wall forming a capillary passage, means for applying a discharge voltage between spaced regions along the length of the interior wall while a dielectric ionizable substance is between the regions, the dielectric substance including at least one element that is ionized to form a plasma in response to the discharge voltage being 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 respectively open and blocked while the discharge voltage is applied between the spaced regions to respectively enable and prevent the flow of plasma through them, the plasma forming an electric discharge channel between the spaced regions while the discharge voltage is applied between the regions, ohmic dissipation occurring in the electric discharge channel in response to the discharge voltage being applied between the regions to produce a high pressure in the passage to cause the plasma in the passage to flow longitudinally in the passage and through the first end to form the pulsed plasma jet.

4. The apparatus of claim 3 wherein the interior wall is solid and includes the dielectric ionizable substance and the element is ablated and ionized from the solid to form the plasma.

5. The structure of claim 3 wherein the voltage applying means includes a first electrode forming the first end and a second electrode plugging the second end while the discharge is occurring.

6. Apparatus for accelerating a projectile comprising means forming a confined path having a longitudinal axis along which the projectile traverses, and means for supplying a pulsed high pressure, high velocity plasma jet to the path from outside the path and to the rear of the projectile as the projectile traverses the path to accelerate the projectile along the path, the jet entering the confined path at a non-zero acute angle relative to the confined path axis, a plurality of the supplying means being located at spaced longitudinal regions along the path, and means for synchronizing the activation of the jets at each of the spaced regions so that at each of the longitudinal regions a pulse of the high pressure, high velocity plasma is applied to the rear of the projectile immediately after the projectile has traversed each of the longitudinal regions, the projectile and confined path geometries being such that the high velocity plasma applied to the rear of the projectile leaks around the projectile so some of the plasma is in front of the projectile to tend to impede acceleration of the projectile in the path, and means between at least some of said spaced longitudinal regions for venting the plasma leaking around the projectile from the confined path.

7. The apparatus of claim 6 wherein the means for venting includes perforations in the confined path, the perforations between each adjacent pair of longitudinal regions having an area approximately twice the cross sectional area of the interior of the confined path.

8. The apparatus of claim 6 wherein the confined path has a circular interior cross section and the projectile is shaped as a surface of revolution having a maximum diameter slightly less than the diameter of the circular interior cross section, the means for venting including perforations in the confined path, the perforations between each adjacent pair of longitudinal regions having an area approximately twice the cross sectional area of the interior of the confined path.

9. Apparatus for accelerating a projectile comprising means forming a confined path having a longitudinal axis along which the projectile traverses, means for accelerating the projectile from rest in the path, a plurality of cascaded intermediate velocity stages for accelerating the projectile from non-free to free flight in the path downstream of the means for accelerating from rest, a plurality of cascaded high velocity stages for accelerating the projectile in the path downstream of the plural intermediate stages, each of the intermediate stages including means for applying a pulsed plasma jet to the rear of the projectile, each of the high velocity stages including means for supplying plasma to the sides of the projectile as the projectile traverses the particular high velocity stage.

10. The apparatus of claim 9 wherein the pulsed plasma jet applying means of each intermediate stage includes means for supplying the jet to the path from outside the path, the jet entering the confined path at a non-zero acute angle relative to the axis.

11. The apparatus of claim 10 wherein the means for supplying the jet from outside the path includes a capillary tube having a longitudinal axis displaced from the confined path axis by said angle, the tube having an inner wall including a dielectric ionizable substance, and means for applying a voltage between spaced points along the tube longitudinal axis to the substance so that the substance is ionized to form the plasma inside of the tube, the tube being dimensioned so that the plasma formed therein has a high velocity and high pressure to form each of the jets, the tube having a closed first end while the voltage is applied between the spaced points and a second end having an orifice into the confined path, the tube longitudinal axis being displaced from the confined path by said angle so that the jet associated with the supplying means propagates along the longitudinal axis of the tube and through the orifice into the confined path generally in the same direction as the projectile is being accelerated.

39. The apparatus of claim 9 wherein each of the means for applying a pulsed plasma jet to the rear of the projectile includes means for supplying at least one longitudinally propagating plasma stream to a longitudinal location of the path, said at least one plasma jet stream having force components in line with the axis when the jet stream is behind the projectile in the confined path to accelerate the projectile.

40. The apparatus of claim 9 wherein each of the means for applying a pulsed plasma jet to the rear of the projectile includes means for simultaneously supplying N longitudinal plasma jets to a common longitudinal location of the path, where N is an integer greater than 1, each of said plasma jets having substantially the same pressure and velocity as well as a common angular displacement in the direction of the longitudinal propagation thereof from the axis of the confined path and being symmetrically disposed relative to the axis of the confined path so that transverse force components of the plasma jet streams relative to the axis are substantially cancelled and force components of the plasma jet streams combine behind the projectile, the in line additive components combining behind the projectile in the confined path to accelerate the projectile.

41. The apparatus of claim 9 wherein each of the means for applying a pulsed plasma jet to the rear of the projectile includes means for supplying at least one longitudinally propagating plasma stream to a longitudinal location of the path, said at least one plasma jet stream having force components in line with the axis when the jet stream is behind the projectile in the confined path to accelerate the projectile.

12. Apparatus for accelerating a projectile comprising means forming a confined path having a longitudinal axis along which the projectile traverses, and means for supplying a pulsed high pressure, high velocity plasma jet to the path from outside the path and to the rear of the projectile as the projectile traverses the path to accelerate the projectile along the path, the jet entering the confined path at a non-zero acute angle relative to the confined path axis, the means for supplying comprising a tube having a longitudinal axis displaced from the confined path axis by the acute angle, the tube having an inner diameter including a dielectric ionizable substance, and means for applying a discharge voltage to the substance between displaced regions along the tube longitudinal axis to cause the substance to be ionized to form the plasma inside of the tube, the tube being dimensioned so that the plasma formed therein in response to the discharge voltage has a high velocity and high pressure to form the jet, the tube having a closed first end while the plasma is formed therein and a second end including an orifice into the confined path, the tube longitudinal axis being displaced from the confined path by said angle so that the jet propagates along the longitudinal axis of the tube and through the orifice into the confined path generally in the same direction as the projectile is being accelerated.

13. The apparatus of claim 12 wherein the angle is approximately 15°

.

14. The apparatus of claim 12 wherein the substance is a solid that is ablated to form the plasma in response to the substance being ionized.

15. The apparatus of claim 14 wherein the ionizable substance includes a hydrogen rich, carbon hydrogen composition, the hydrogen and carbon in the composition being ionized in response to the applied voltage to form the plasma.

16. A method of accelerating a projectile along a confined path having a longitudinal axis along which the projectile traverses, comprising supplying a pulse of high pressure, high velocity plasma to the path behind the projectile as the projectile traverses the path by supplying a jet of the plasma to the confined path from a source located outside of the confined path so the plasma enters the path at a non-zero acute angle relative to the axis, the jet being derived by applying an electric discharge between spaced regions along a longitudinal axis of a capillary passage, blocking one end of said passage while the discharge is occurring, an electric discharge channel being formed by the plasma in the passage between the spaced regions in response to the applied electric discharge, ohmic dissipation occurring in the electric discharge channel in response to the applied electric discharge to produce a high pressure in the passage to cause plasma to flow longitudinally in the passage and through an orifice in an end of the passage opposite from the blocked one end, the plasma flowing through the orifice into the confined path to form the jet.

17. The method of claim 16 further including accelerating the jet while it is in the passage to several times the sound speed of plasma in the jet so that the jet has a velocity in the confined path of approximately twice the projectile velocity while the jet acts against the rear of the projectile.

18. The method of claim 16 further including expanding and cooling the jet as it enters the confined path.

19. The method of claim 18 further including supplying additional material to the passage to replace plasma supplied by the passage to the confined path while the plasma is ejected from the passage into the confined path, and bombarding a wall of the passage with radiation from the plasma.

20. The method of claim 16 wherein the jet is derived by ablating material from an interior dielectric tube wall forming the passage in response to the applied electric discharge.

21. The method of claim 20 further including ablating additional material from the wall to replace plasma ejected from the wall into the confined path while the plasma is ejected from the wall into the confined path, and bombarding the wall with radiation from the plasma.

22. The method of claim 16 wherein the plasma pulse is supplied to the rear of the projectile to impart kinetic energy to the projectile to accelerate the projectile along the path.

23. The method of claim 22 wherein N of the plasma jets are simultaneously supplied to a common longitudinal location of the path, where N is an integer greater than 1, each of said jets having substantially the same pressure and velocity, the in line additive force components of the plasma jets combining behind the projectile in the confined path to accelerate the projectile.

24. Apparatus for accelerating a projectile comprising means forming a confined path having a longitudinal axis along which the projectile traverses, and means for supplying a pulsed high pressure, high velocity plasma jet to the path from outside the path and to the rear of the projectile as the projectile traverses the path to accelerate the projectile along the path, the jet entering the confined path at a non-zero acute angle relative to the confined path axis, the supplying means including a capillary passage having a longitudinal axis, said passage having one closed end and an orifice at the other end into the confined path, means for applying a discharge voltage between spaced longitudinal regions of the passage in the direction of the passage longitudinal axis to form a plasma in the passage, an electric discharge channel being formed by the plasma in the passage between the spaced passage regions while the discharge voltage is applied between the spaced regions, said one end being closed while the discharge is occurring, ohmic dissipation occurring in the electric discharge channel while the discharge voltage is applied between the spaced regions to produce a high pressure in the passage to cause plasma to flow longitudinally in the passage and through the orifice to form the jet that enters the confined path.

25. The apparatus of claim 24 wherein the supplying means includes a tube having an interior dielectric wall forming the capillary passage, the wall containing plasma forming material which is ablated in response to the discharge voltage being applied between the spaced regions.

26. The apparatus of claim 24 wherein the confined path and capillary passage are in a vaccum.

27. The apparatus of claim 24 wherein said supplying means includes means for supplying at least one longitudinally propagating plasma jet stream to a longitudinal location of the path, said at least one plasma jet stream having force components in line with the confined path axis when the jet stream is behind the projectile, the in line additive components combining behind the projectile in the confined path to accelerate the projectile.

28. The apparatus of claim 24 wherein said supplying means includes means for simultaneously supplying N longitudinally propagating plasma streams to a common longitudinal location of the path, where N is an integer greater than 1, each of said plasma jet streams having substantially the same pressure and velocity as well as a common angular displacement in the direction of the longitudinal propagation thereof from the axis of the confined path and being symmetrically disposed relative to the axis of the confined path so that transverse force components of the plasma jet streams relative to the axis are substantially cancelled and force components in line with the axis that are additive when the plasma jet streams combine behind the projectile, the in line additive components combining behind the projectile in the confined path to accelerate the projectile.

29. The apparatus of claim 24 wherein said supplying means includes means for supplying a longitudinally propagating plasma stream to a particular longitudinal location of the path via asymmetrically located nozzle means for producing asymmetric force components transverse to the axis at the particular location where the jet stream enters the path in response to the jet stream, the jet stream being timed so that it enters the path at a time when the projectile is downstream of the nozzle means, the plasma stream flowing through the nozzle means having in line and transverse components relative to the axis of the path, the in line components adding to combine behind the projectile in the confined path to accelerate the projectile, the projectile location at the time the plasma stream enters the path being such that transverse components are not applied by the plasma to the projectile.

30. The apparatus of claim 24 wherein the confined path is configured and the jet is oriented to enter the confined path so that the jet supplies kinetic energy to the rear of the projectile to accelerate the projectile along the path.

31. The apparatus of claim 24 wherein the confined path has a circular interior cross section and the projectile is shaped as a surface of revolution having a maximum diameter slightly less than the diameter of the circular interior cross section.

32. The apparatus of claim 24 wherein the capillary passage includes an outwardly flared nozzle through which the jet is injected into the confined path so the jet expands and cools as it enters the confined path.

33. The apparatus of claim 24 wherein the confined path has a cross-sectional area considerably greater than the cross-sectional area of the capillary passage so the jet expands and cools as it enters the confined path.

34. The apparatus of claim 33 wherein the capillary passage includes an outwardly flared nozzle through which the jet is injected into the confined path so the jet expands and cools as it enters the confined path.

35. The apparatus of claim 24 wherein a plurality of the supplying means are located at spaced longitudinal regions along the path, and means for synchronizing the activation of the jets at each of the spaced regions so that at each of the longitudinal regions a pulse of the high pressure, high velocity plasma is applied to the rear of the projectile after the projectile has traversed that longitudinal region.

36. The apparatus of claim 35 wherein said means for synchronizing includes means for detecting movement of the projectile at a point upstream of one of said regions, and means responsive to the detecting means signalling movement of the projectile through the point for activating a jet applied to one of the regions downstream of the point.

37. The apparatus of claim 24 wherein a plurality of said supplying means are located at spaced longitudinal regions along the path, and means for activating the jets at a plurality of the spaced regions so that at each of the plural spaced longitudinal regions a pulse of the high pressure, high velocity plasma is applied to the rear of the projectile immediately after the projectile has traversed each of the longitudinal regions.

38. The apparatus of claim 37 wherein the means for activating at at least some of the plural spaced regions includes means for detecting movement of the projectile at a point upstream of each of said at least some regions, and means responsive to the detecting means signalling movement of the projectile through the points for activating the jets applied to the regions downstream of the points, the geometry of the projectile and confined path being such that plasma has a tendency to leak around the projectile so some of the plasma is in front of the projectile, the plasma in front of the projectile tending to accumulate and to impede the acceleration of the projectile, and means between said at least some of the spaced longitudinal regions and the points for detecting movement immediately downstream of each longitudinal region for venting the plasma in front of the projectile from the confined path.