FIELD: salvo-fire jet projectiles. SUBSTANCE: tail plane stabilizer has opening arched blades installed on the fairing. The front and rear edges of the blades have an asymmetric shape with a bevel on the convex surface of the blade. The relation between the bevel width in the direction perpendicular to the edges and the blade thickness perpendicular to the edges and the blade thickness makes up 2 to 6, and the span of the stabilizer blades is made within 1.2 to 1.6 of the blade root chord. EFFECT: increased range of projectile fire, enhanced reliability and fire efficiency of the projectile due to the decreased range of variation of the spin rate and prevented resonance phenomena in flight. 1 dwg
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Authors
Dates
2001-11-20—Published
2001-03-20—Filed