ROCKET SOLID PROPELLANT CHARGE Russian patent published in 2003 - IPC

Abstract RU 2216641 C1

FIELD: rocketry. SUBSTANCE: proposed charge proper rigidly connected with housing and protective-and-fastening layer playing the part of heat protective coating and fastening layer. Protective-and-fastening layer of thickness equal to 0,1•10-2-2,5•10-2 of outer diameter of charge, being essentially sheet calendared material of basis of ethylene-propylene-diene rubber with chrysolite asbestos filler, contains also dioctyl sebacate in amount of 3-300 mass parts and para- dinitrosobenzene in amount of 2-10 mass parts. EFFECT: provision of rocket solid propellant charge reliably connected with rocket engine by one protective-and-fastening layer playing the part of heat protective coating and fastening layer. 1 tbl, 3 dwg

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RU 2 216 641 C1

Authors

Valeev N.S.

Zvereva I.G.

Amarantov G.N.

Baranov G.N.

Shamraev V.Ja.

Kusakin Ju.N.

Talalaev A.P.

Solov'Ev A.F.

Kuz'Mitskij G.Eh.

Fedchenko N.N.

Vronskij N.M.

Makarov L.B.

Bulashevich A.P.

Ezhov G.P.

Fokin A.S.

Okhrimenko Eh.F.

Kolesnikov V.I.

Dates

2003-11-20Published

2002-06-24Filed