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US 4,357,611 AGranted
Radar cross section augmentation
AssigneeThe United States of America as represented by the Secretary of the Air Force
InventorEdward N. Skomal
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AssigneeThe United States of America as represented by the Secretary of the Air Force
InventorEdward N. Skomal
Estimating the term…
Structural improvement for, and method of, achieving radar cross section augmentation of a conical reentry space vehicle decoy having a dielectric heatshield by structuring the base of the decoy to meet certain conditions. Augmentation is achieved by structuring the decoy to have at the base a reflecting step with a 90 degree angle formed by the internal surface of heatshield and the surface of the base portion of the heatshield, where the dielectric constant of the heatshield is in a range of values predetermined by use of the equation: .epsilon..gtoreq.2(1+tan .alpha.)+tan.sup.2 .alpha., where .epsilon.=the dielectric constant of the heatshield, and .alpha.=the half angle cone of the conical decoy. Any incident radar signal impinging in a nose-on direction upon the external surface of the heatshield enters the heatshield, is completely double reflected within the reflecting step of the heatshield, and is re-directed out of the heatshield and in the opposite direction (i.e., in the direction of the nose of the decoy). The forward (i.e., nose-on) radar cross section of the decoy is thereby significantly augmented, without the appendages, external of the decoy, that are required by the prior art.
In a conical reentry vehicle having a geometric axis, a half cone angle, and a dielectric heatshield with an external surface, an internal surface, a forward portion with a nose, and a base portion with a surface, wherein the reentry vehicle has a radar cross section and the dielectric heatshield has a predetermined dielectric constant, the improvement comprising a reflecting step at the base portion of the heatshield, with the reflecting base step having a base step angle formed by, and at, the intersection of the internal surface of the heatshield and the surface of the base portion of the heatshield, and with the reflecting base step shaped to produce two total double reflections, internal of the heatshield, of any incident radar signal impinging in a nose-on attitude and direction upon the external surface of the heatshield and entering the heatshield, whereby the double reflected signal is re-directed outward from, and emerges outward of, the heatshield in the direction of the nose of the reentry vehicle, thereby increasing the nose-on radar cross section of the reentry vehicle.
The method of augmenting a radar cross section of a conical reentry space vehicle having a radar cross section, a geometric axis, a half cone angle, and a dielectric heatshield having a dielectric constant, a forward portion with a nose, an external surface, an internal surface, and a base portion with a surface, comprising the step of forming a reflecting base step having a base step angle of a magnitude of 90 degrees, wherein said base step angle is formed by, and at, the intersection of the internal surface of the heatshield and the surface of the base portion of the heatshield, and wherein the dielectric constant of the heatshield is in a range of values predetermined by the use of the equation:
Dependencies are inferred from the claim text.