HOUSING OF SOLID-PROPELLANT ROCKET ENGINE Russian patent published in 2003 - IPC

Abstract RU 2218472 C1

FIELD: rocketry. SUBSTANCE: proposed housing of solid-propellant rocket engine contains cylindrical shell, end parts including adapter and threaded sections. Thickness of cylindrical shell and thickness of threaded section are equal, respectively, to 0.18- 0.25 and 0.4-0.6 of thickness of adapter section. Inner diameter of cylindrical shell inner diameter of threaded section are equal, respectively, to 1.04-1.05 and 1.01- 1.05 of inner diameter of adapter section. Ultimate strength of threaded and adapter sections is equal to 0.55-0.90 of ultimate strength of cylindrical shell. EFFECT: provision of reliable functioning of rocket projectile with such engine owing to rational design parameters of housing of solid propellant rocket engine. 1 dwg

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RU 2 218 472 C1

Authors

Tarasov A.I.

Uglov V.M.

Makarovets N.A.

Denezhkin G.A.

Semilet V.V.

Tregubov V.I.

Kashirkin A.A.

Peturkin D.M.

Filatov V.G.

Aljazhedinov V.R.

Sobko V.F.

Dates

2003-12-10Published

2003-02-06Filed