Method and apparatus for launching a projectile at hypersonic velocity

• US 4,932,306 A
• Filed: 02/18/1988
• Issued: 06/12/1990
• Est. Priority Date: 04/13/1987
• Status: Expired due to Fees

• Current Assignee: Josef Rom
• Original Assignee: Josef Rom
• Inventors: Rom, Josef
• Primary Examiner(s): BENTLEY, STEPHEN
• Application Number:
  US07/157,472
• Time in Patent Office: 845 Days
• Field of Search: 89/8, 244/63
• US Class Current: 89/8
• CPC Class Codes: F41A 1/04 Missile propulsion using the combustion of a liquid, loose powder or gaseous fuel, e.g. hypergolic fuel
• CPC Class Codes: F42B 10/04 using fixed fins F42B10/22 takes precedence

Abstract

A projectile is accelerated to hypersonic velocity in an initially closed barrel of a diameter considerably larger than the projectile diameter which is filled with a compressed fuel-oxidizer mixture. The projectile comprises a conical nose portion, an intermediate portion formed to generate oblique detonation waves, and a tapering tail portion provided with several radial vanes. The projectile is propelled by an initiator gun at supersonic speed through one of the intitially closed ends in the barrel, were the detonation waves cause detonation and combustion of the fuel-oxidizer mixture. The detonation results in a high pressure increase to the rear of the projectile accelerating it along the barrel and shooting it at the reached hypersonic speed through the other, initially closed end of the barrel into the open.

Claims

1. A method of accelerating a body to a high velocity, comprising the steps of:

filling an oblong vessel with a compressed fuel-oxidizer mixture, said oblong vessel having initially closed ends and having a large inner diameter compared with outer dimensions of said body,

propelling said body at supersonic velocity into said oblong vessel, said body generating bow shock waves and oblique detonation waves said bow shock waves and said oblique detonation waves intersecting and interacting within said oblong vessel prior to reaching an inner wall of said oblong vessel,

detonating said fuel-oxidizer mixture with said oblique detonation waves causing forward thrust and acceleration of said body by pressure generated by denotation of said fuel-oxidizer mixture and expansion of high-pressure gases to the rear of said body.

2. A body propelled by the method as claimed in claim 1, having a nose portion in the shape of waverider of known design such as a planar Caret Wing, characterized by the addition of a tail portion of rearwardly diminishing cross section, and by the provision of a sharp edge at the border between said nose portion and said tail portion, adapted to generate detonation shock waves.

3. An axisymmetrical body propelled by the method as claimed in claim 1, comprising a long nose cone, a plurality of radial vanes of gradually increasing height integral with said nose cone, and a tail portion in the shape of a taper decreasing in diameter to a point at the rear end of said body.

4. The body of claim 3, comprising a conical nose portion, an intermediate portion, and a tapering tail portion, characterized by the provision of a plurality of radial vanes extending the entire length of said body, and by the provision on said intermediate portion of means adapted to generate oblique detonation waves.

5. The body of claim 4, comprising means for generating oblique detonation waves in the shape of a forward facing step on said intermediate portion.

6. The body of claim 4, comprising means for generating oblique detonation waves, in the shape of a ramp provided around said intermediate portion.

7. The body of claim 4, comprising means for generating oblique detonation waves in the shape of pyrotechnical means incorporated in said body.

8. The body of claim 4, comprising means for generating oblique detonation waves in the form of laser radiation means incorporated in said body.

9. The body of claim 4, provided with inclined vanes in said tail portion adapted to impart a spinning motion to said body.

10. The body of claim 4, provided with sideways directed jet means adapted for steering and maneuvering said body.

11. The body of claim 10, provided with target detecting means and jet operating means adapted to direct said body onto a target.

12. The body of claim 4, comprising means for generating oblique detonation shock waves in the form of a skirt surrounding said intermediate portion and at least part of said tail portion in spaced-apart alignment.

13. The body of claim 12, wherein said skirt extends between the outer edges of the fins of said tail portion.

14. The body of claim 13, wherein said skirt in the shape of a hollow cylinder.

15. The body of claim 13, wherein said skirt is in the shape of planar sheets extending between the outer edges of each two adjacent fins.

16. The body of claim 4, comprising a skirt adapted to be detached from said body after this has been expelled out of said oblong vessel.

17. An acceleration system comprising:

a first vessel filled with a combustible fluid;

a projectile, said projectile including a first wave generation means for generating a first wave and a second wave generation means for generating a second wave, said first wave and said second wave interacting, prior to reflecting off an inner wall of said first vessel, to cause detonation of said combustible fluid; and

a tail, attached to said projectile, which directs combustion products resulting from said detonation of said combustible fluid so that said projectile is accelerated.

18. An acceleration system as set forth in claim 17, wherein

said first wave is a bow shock wave and said second wave is an oblique detonation wave.

19. An acceleration system as set forth in claim 17, further comprising:

a gun which imparts an initial motion on said projectile such that said projectile is moving at a high rate of speed as said projectile enters said first vessel.

20. An acceleration system as set forth in claim 18, wherein

said first wave raises the temperature of said combustible fluid to a temperature below a detonation point of said combustible fluid;

and wherein

said second wave raises the temperature of said combustible fluid to a temperature above said detonation point of said combustible fluid.

21. An acceleration system as set forth in claim 19, further comprising:

a second vessel filled with a combustible fluid, said first vessel and said second vessel being arranged so that said first vessel is in line with said gun during a first time period and said second vessel is in line with said gun during a second time period.

22. An acceleration system as set forth in claim 19, further comprising:

a first membrane located at a first end of said first vessel; and

a second membrane located at a second end of said first vessel;

wherein

said fluid is a fuel-oxidizer gas mixture; and

wherein

said gun shoots said projectile through said first membrane into said first vessel at supersonic velocity, and said projectile exits said first vessel through said second membrane.

23. An acceleration system as set forth in claim 20, wherein

said first wave generation means is a nose of said projectile;

and wherein

said second wave generation means is a forward facing step in a surface of said projectile.

24. An acceleration system as set forth in claim 20, wherein

said first wave generation means is a nose of said projectile;

and wherein

said second wave generation means is a sharp edge in a surface of said projectile.

25. An acceleration system as set forth in claim 20, wherein

said first wave generation means is a nose of said projectile;

and wherein

said second wave generation means is a ramp in a surface of said projectile.

26. An acceleration system as set forth in claim 20, wherein

said first wave generation means is a nose of said projectile;

and wherein

said second wave generation means is a planar surface of a skirt;

said planar surface arranged such that said planar surface is not at a blunt angle with respect to a direction of travel of said projectile.

27. An acceleration system as set forth in claim 20, wherein

said first wave generation means is a nose of said projectile;

and wherein

said second wave generation means is a pyrotechnic device.

28. An acceleration system as set forth in claim 20, wherein

said first wave generation means is a nose of said projectile;

and wherein

said second wave generation means is an electrical device.

29. An acceleration system as set forth in claim 20, wherein

said first wave generation means is a nose of said projectile;

and wherein

said second wave generation means is a light emitting device.

30. An acceleration system as set forth in claim 21, further comprising:

third through N-th vessels each filled with a combustible fluid, said third through N-th vessels successively brought in line with said gun, where N is an integer.

31. A method of accelerating a projectile comprising the steps of:

(a) injecting said projectile into a space filled with a combustible fluid in a first direction, said space being at least partially enclosed by a barrel;

(b) generating a first wave from a first portion of said projectile;

(c) generating a second wave from a second portion of said projectile, said second wave reacting with said first wave, prior to said second wave reflecting off an inner wall of said barrel and prior to said first wave reflecting off said inner wall of said barrel, to detonate said combustible fluid and to produce combustion products; and

(d) directing said combustion products to accelerate said projectile in said first direction.

32. A method of accelerating a projectile as set forth in claim 31 above wherein

step (b) includes raising the temperature of said combustible fluid to a temperature below a detonation point of said combustible fluid;

and wherein

step (c) includes raising the temperature of said combustible fluid to a temperature above said detonation point of said combustible fluid.

33. A method of accelerating a projectile as set forth in claim 31 above wherein

step (b) includes raising the temperature of said combustible fluid to a temperature below a detonation point of said combustible fluid;

and wherein

step (c) includes raising the temperature of said combustible fluid using a pyrotechnic device to a temperature above said detonation point of said combustible fluid.

34. A method of accelerating a projectile as set forth in claim 31 above wherein

step (b) includes raising the temperature of said combustible fluid to a temperature below a detonation point of said combustible fluid;

and wherein

step (c) includes raising the temperature of said combustible fluid using an electrical device to a temperature above said detonation point of said combustible fluid.

35. A method of accelerating a projectile as set forth in claim 31 above wherein

step (b) includes raising the temperature of said combustible fluid to a temperature below a detonation point of said combustible fluid;

and wherein

step (c) includes raising the temperature of said combustible fluid using a light emitting device to a temperature above said detonation point of said combustible fluid.