SOLID-PROPELLANT ROCKET ENGINE Russian patent published in 2005 - IPC

Abstract RU 2245450 C1

FIELD: rocketry.

SUBSTANCE: proposed solid-propellant rocket engine includes channel charge secured to case and to end faces by means of collars which have bulges in their necks. Size of this bulge is 1.5-2.5 of collar thickness along generatrix of neck at neck outlet. Angle formed by bulge surface directed to propellant and axis of charge channel ranges from 45 to 90 deg.

EFFECT: maximum volume occupied by propellant; avoidance of defects in charging.

4 dwg

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RU 2 245 450 C1

Authors

Kolesnikov V.I.

Amarantov G.N.

Talalaev A.P.

Shamraev V.Ja.

Dmitriev A.F.

Lazebnyj V.N.

Vronskij N.M.

Fedchenko N.N.

Guseva G.N.

Gramenitskij M.D.

Bytskevich V.M.

Chub S.I.

Volkov O.K.

Kuz'Mitskij G.Eh.

Dates

2005-01-27Published

2003-06-24Filed