ROCKET ENGINE FOR ARTILLERY PROJECTILE Russian patent published in 1994 - IPC

Abstract RU 2021544 C1

FIELD: artillery engineering. SUBSTANCE: ignitor 4 is positioned on plug within conical casing 3 and provided with delayer 5 mounted from the side of nozzle exit. Stabilizers 9 overlap face of delayer 5. A member that fixes the plug is made of pipe 12 whose one end is secured to nozzle 1 at its throat section and the other end is provided with projections 17 which enclose the casing of ignitor 5. EFFECT: enhanced reliability. 2 dwg

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RU 2 021 544 C1

Authors

Sokolov G.F.

Mironov Ju.I.

Berkovich V.S.

Dates

1994-10-15—Published

1992-04-07—Filed