CHARGE OF SOLID PROPELLANT FOR ROCKETS

FIELD: rocketry. ^ SUBSTANCE: proposed solid-propellant charge with radial channel contains case made with radius generatrix in front part and protective and fastening layer. Interslot projections of radial section of channel intersect partially space made at front end face of charge. Charge channel...

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Bibliographische Detailangaben
Hauptverfasser:	AMARANTOV G.N, KORENNOJ A.V, SHVYKIN JU.S, DUDKA V.D, VASINA E.A, KOLIKOV V.A, TALALAEV A.P, MAKAROV L.B, KUZ'MITSKIJ G.EH, PLOTNIKOVA T.N, VRONSKIJ N.M, FILIMONOV G.D, MOROZOV V.D, SURNACHEV A.F, KOLESNIKOV V.I, SHIPUNOV A.G, PICHKALEV ZH.A, SHATROVA EH.A, KOLACH P.K, FEDCHENKO N.N
Format:	Patent
Sprache:	eng ; rus
Schlagworte:	BLASTING COMBUSTION ENGINES HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS JET-PROPULSION PLANTS LIGHTING MECHANICAL ENGINEERING WEAPONS
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Beschreibung
Zusammenfassung:	FIELD: rocketry. ^ SUBSTANCE: proposed solid-propellant charge with radial channel contains case made with radius generatrix in front part and protective and fastening layer. Interslot projections of radial section of channel intersect partially space made at front end face of charge. Charge channel is made cylindrical at rear end face. Interslot projections are made with height decreasing in length and terminating at distance not less than two diameters of cylindrical section of channel from rear end face of charge. Invention makes it possible to improve reliability of functioning of optical command control system owing to decrease of formation of smoke at combustion of charge. ^ EFFECT: reduced mass of remaining charge, increased volume filling of combustion chamber. ^ 2 dwg