This idea is not new, but I guess this is the time to share it. I have applied for 4 patents regarding the design details of this interceptor. It relies on a pressure-fed rocket architecture; instead of turbopumps, the pressure of the fuel tanks pushes the fuel to the rocket engine. The interceptor utilizes my trademark unified engine block, Tesla Valves, regenerative cooling canals, and a low-pressure combustion chamber with a slit exit nozzle.
This engine design allows even low-pressure tanks to run the rocket. The propellants (LNG and LOX) regeneratively heat up, and the Tesla Valve ensures the pressure of the gasified fuel is higher than the pressure of the liquid propellant. As with my other designs, the engine is optimized for maximum air augmentation. The Tesla Valve ensures pulsed exhaust, and the lack of a traditional nozzle allows for a slightly more divergent exhaust gas. Both are ideal for optimal air mixture. By maximizing the air augmentation and afterburner effect, the rocket carries less LOX on board and, with the same fuel, attains higher speeds and longer ranges. Air augmentation and ambient oxygen increase the Iₛₚ of the rocket, similar to high-bypass turbofan engines, though in a much more compact, light, and agile engine.
In order to maximize the air augmentation, the interceptor has a void on its nose. This air intake increases towards the back of the rocket, lowering its pressure where the intake air meets the engine exhaust gas. The interceptor's aft is curved to allow more air to flow due to the Coandă effect, further increasing the augmented air.
To reduce the weight of the rocket—which requires stronger fuel tanks due to internal pressure—I opted for a Gradient Hexagonal Design. This increases strength with minimal weight penalty. The smaller hexagonal structures on the outer skin double as coolant reservoirs (for high Mach numbers) and shrapnel shields. The propellant is distributed among independent hexagonal structures traversing from the nose to the aft. As a result, any puncture leads only to a small fuel loss. Additionally, these hexagonal tanks have Tesla-valve-like vertical structures in them. These valves reduce liquid fuel sloshing, prevent liquid from flowing to the nose instead of the aft, and increase structural strength due to their perpendicular position compared to the horizontal hexagonal tanks. As a result, the interceptor can perform much higher G-maneuvers without breaking.
The major difference of my interceptor from others is its shape. It has a hexagonal structure instead of a tubular one. This geometry provides the interceptor with passive stability, negating the need for fragile fins and external stabilizers. More importantly, this design acts like a wing and increases lift. Therefore, the interceptor spends less fuel to counteract gravity, which increases its range even further.
One final and important design feature is its nose. The nose is not a monolithic structure like the rest of the interceptor; it is made of six trapezoidal mini-interceptors. When the target is close, these mini-interceptors fire their engines and split away from the main body. As a result, a single interceptor can hit 6 + 1 = 7 targets. This is a very important feature when intercepting cheap drones or missiles, as it significantly reduces the cost of intercepting a target. The trapezoidal design of the mini-interceptors allows for passive stabilization and lift, just like the main body. Their curved aft sections also allow them to utilize air augmentation.
Finally, the monolithic structure with a smooth surface (no protrusions) allows for compact piling of the interceptors, negating the need for racks and maximizing transport efficiency.








