Missile Decoy Radar Cross Section Enhancer.
Patent, Filed 17 Oct 79, patented 13 Oct 87,
DEPARTMENT OF THE AIR FORCE WASHINGTON DC
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A decoy missile having the shape of a reentry vehicle and containing a pair of conically shaped dipole jacks in tandem, the jacks are shaped and spaced to provide a desired reflective cross section at a specific frequency, the rear cover plate of the decoy is constructed of radar absorbing material to aid in the enhancement process.
- Guided Missile Reentry Vehicles