| 摘要 |
1. A shaped charge engine, comprising: an inner housing; an outer housing joined to the inner housing to define a blast-forming chamber; a plurality of fuel injectors adapted to inject fuel into the chamber at generally diametrically opposite locations; and a central opening in the blast-forming chamber between the inner and outer housings defining a primary convergence zone; whereby exhaust gases traveling through the primary convergence zone from generally opposite locations collide at a secondary convergence zone substantially at the center of the shaped charge engine to produce a hypersonic exhaust. 2. The shaped charge engine of claim 1, wherein the inner housing is generally annular in shape and includes a substantially conical convex projection that, together with the outer housing, forms the primary convergence zone. 3. The shaped charge engine of claim 1, wherein the outer housing is substantially dome-shaped. 4. The shaped charge engine of claim 1, wherein the inner and outer housings constructed of a non-circular, polygonal cross-sectional shape from a perspective orthogonal to the exhaust direction. 5. The shaped charge engine of claim 1, wherein the blast-forming chamber is comprised of a plurality of generally opposed sub-chambers, each of which includes a fuel injector and igniter. 6. The shaped charge engine of claim 6, wherein the generally opposed sub-chambers are pivotable in the vicinity of the apex of the outer housing to enable the orientation of the sub-chambers to be varied between a position that directs initial exhaust products in a direction at an obtuse angle with the direction of final exhaust through a position that directs initial exhaust products in a direction at an acute angle with the direction of final exhaust. 7. The shaped charge engine of claim 6, wherein the inner housings of the sub-chambers further comprise projections adjustably attached to the inner housing so that the projections may be moved toward or away from the outer housing to decrease or increase the size of a pinch point defining the primary convergence zone. 8. The shaped charge engine of claim 1, further comprising a plurality of igniters extending at least partially into the chamber and a source of oxygen, whereby a spark or flame from the igniters causes fuel ignition. 9. The shaped charge engine of claim 8, further comprising a mass injector projecting at least partially into the chamber and connected to a mass source, the mass injector adapted to inject mass into the chamber following fuel combustion. 10. The shaped charge engine of claim 8 wherein the mass comprises water. 11. The shaped charge engine of claim 9, wherein the source of oxygen comprises separate sources of air and oxidizer. 12. The shaped charge engine of claim 11, further comprising a sensor to detect the available presence of air mass and a controller in communication with the sensor to adjust the delivery of oxygen to the chamber from all air to all oxidizer or a mixture of air and oxidizer.
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