FIELD: weapons.
SUBSTANCE: invention concerns military equipment, particularly missiles and jet missiles of fuel/air explosive effect. Missile includes payload with detonating charge placed in case, bottom fuse and firing explosive charge positioned in tubular case. Fuel/air explosive charge features liquid components, and payload case is elongated. Front payload end at propulsion motor side is closed by cover on cap shape mounted in payload case with concave side oriented towards fuel/air explosive charge. Seam sealing elements in the form of rubber rings in annular grooves on cover are positioned between cover and payload case. Annular lug is made at inner surface of payload case around cover in sealing element location, and cover features through axial orifice for cover installation onto bottom fuse and firing explosive charge case. External surface of bottom fuse and firing explosive charge features annular lug, and cover rests against the lug and is tightened rigidly to it by nut screwed to bottom fuse and firing explosive charge case. Firing explosive charge is tightened to annular lug of the tube in front of bottom fuse at propulsion motor side by nut screwed into its case.
EFFECT: high efficiency and sensitivity of actuated fuel/air explosive charge.
3 dwg
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Authors
Dates
2009-05-27—Published
2007-07-13—Filed