SOLID-PROPELLANT ROCKET CHARGE Russian patent published in 2003 - IPC

Abstract RU 2220312 C1

FIELD: rocketry. SUBSTANCE: proposed solid propellant rocket charge contains housing, end face cups, protective-and fastening layer, head semicharge with star-like channel and tail semicharge with cylindrical channel. Area of through section of inlet part of cylindrical channel of tail semicharge is 1.00-0.25 of area of outlet cross section of star-like channels of head semicharge. Difference in initial thickness of burning arch of head semicharge over length of star-like channel, and difference in initial thickness of burning arch of tail semicharge over length of cylindrical channel is 1.5-3.5 of average thickness of protective-and-fastening layer. Value of standard modulus of elasticity of propellant semicharge at maximum limited temperature of application is chosen within (0.08 kgf/cu.cm and 0.30 kgf/cu. cm)L where L is length of semicharge. EFFECT: provision of reliable functioning of charge with high filling density made of high elasticity propellants featuring high combustion temperature. 1 dwg

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RU 2 220 312 C1

Authors

Kuz'Mitskij G.Eh.

Grinberg S.I.

Makarov L.B.

Lisovskij V.M.

Vronskij N.M.

Makarovets N.A.

Denezhkin G.A.

Talalaev A.P.

Kolesnikov V.I.

Amarantov G.N.

Kolach P.K.

Nekrasov V.I.

Semilet V.V.

Podchufarov V.I.

Tregubov V.I.

Kashirkin A.A.

Koroleva N.B.

Shubkin E.A.

Dates

2003-12-27Published

2003-04-04Filed