ROCKET PART OF JET PROJECTILE Russian patent published in 2000 - IPC

Abstract RU 2158377 C1

FIELD: salvo fire systems. SUBSTANCE: rocket part includes thin-walled case at unit alongation more than 10 calibres and nozzle unit with cylindrical fairing of aerodynamic stabilizer secured on it. Case of rocket part and fairing of aerodynamic stabilizer are provided with at least three circular beads located symmetrically along length of case and fairing, respectively. Diameter and width of circular beads are equal to 1.01-1.02 and 0.15- 0.25, respectively. EFFECT: enhanced stability of flight of projectile at velocities exceeding 4 M. 1 dwg

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RU 2 158 377 C1

Authors

Makarovets N.A.

Denezhkin G.A.

Obozov L.I.

Semilet V.V.

Peturkin D.M.

Filatov V.G.

Sobko V.F.

Druzhinin V.G.

Uglov V.M.

Koval'Chuk V.Ja.

Dates

2000-10-27Published

1999-11-11Filed