ANTIAIRCRAFT GUIDED ROCKET

摘要

ammunition for antiaircraft defense. SUBSTANCE: antiaircraft guided rocket has main stage with body in the form of thin-walled shell joined to head fairing which houses functional units, booster, stage separation mechanism. Telemetry unit with radio transmitter is installed in main stage in point of placement of warhead, optical sensor is positioned at distance h from outer shell of body of main stage on rear butt of transmitter. Hole with diameter D closed air-tight by transparent material is made in shell of body uniaxially to optical sensor and perpendicular to longitudinal axis of rocket. Ratio of distance from outer surface of shell of body to optical sensor to diameter of hole in shell of body lies within bounds described by formula EFFECT: possibility for generation of information on flight of rocket during test rocket firing at training stage. 3 dwg