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>The current rocket engine obtains thrust by a jet injection >method that burns oxygen and fuel, but the next-generation >rocket engine can reduce the size of the rocket engine to 1/10 >in the blast shock wave detonation propulsion that explodes the fuel. >The fastest rocket exhaust speed is the jet injection speed of >a solid rocket, which is the limit at Mach 7, but the detonation >method can obtain an exhaust speed of Mach 8.3, and the discharge >pressure is 10 times or more, that is, conventional It will be >launched by a 1/10 small rocket. >In other words, it enables the image of launching with just >the Space Shuttle itself. This is the next-generation rocket engine.