INDUCTION FLYING BODY

• Main Author: OSAKI MASARU
• Format: Patent
• Language: English
• Published: 26.06.2002
• Edition: 7
• Subjects: AMMUNITION; AMMUNITION FUZES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES; ARMING OR SAFETY MEANS THEREFOR; BLASTING; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION; HEATING; LIGHTING; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION ORRERADIATION OF RADIO WAVES; MEASURING; MECHANICAL ENGINEERING; PHYSICS; RADIO DIRECTION-FINDING; RADIO NAVIGATION; TESTING; WEAPONS

PROBLEM TO BE SOLVED: To provide an induction flying body capable of setting in initiation delay time at which a war nose is capable of accurately destroying a target object. SOLUTION: A target detecting distance calculating circuit is provided to calculate a target detecting distance when a detonating fuse detects approach of a target object through correlation between an approach detonating fuse transmission wave and an approach detonating fuse receiving wave. By calculating an initiation delay time at a timing at which a war nose is initiated by using an approach speed of a target object and an induction flying body, an oscillation angle of a radar antenna, the bullet piece speed of the war nose being the adherent value of the induction flying body, the transmission direction of the approach detonating fuse transmission wave, a distance between the mounting positions of an approach detonating fuse and the war nose, and a target detecting distance calculated by a target detecting distance calculating circuit, setting of an effective initiation corresponding to a target detecting distance when an approach detonating fuse detects the target object is practicable.