FIELD: artillery jet ammunition. SUBSTANCE: cassette nose cone has a master controller, body accommodating a frame with diaphragms and military components, with moving-apart engines having two chambers with headings, nozzle, charges and an exhaust-gas duct. A cross-shaped slot is made in the chamber headings, and the surfaces of the chamber headings engageable with the charges are removed from the nozzle axis at distance L=(0.5-1)d. The distance between the planes passing through the axis of the gas-exhaust duct in the point of joint with the chambers and nozzle axis makes up I=(0.1-0.5)d, where d is nozzle diameter. A pair of adjacent headings is provided with longitudinal adjustable supports positioned for engagement with the diaphragms. The chambers are provided with supporting posts directed between which is the resultant thrust of the moving-apart engine. The supporting posts are shifted to the pair of adjacent headings, and radially adjustable supports with dampers made of flexible material, for instance rubber, are positioned in the zone of the other pair of adjacent headings. EFFECT: enhanced reliability and efficiency of combat employment of cassette nose cones with precise-guidance military components. 2 cl, 9 dwg
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Authors
Dates
2001-04-27—Published
2000-02-29—Filed