INSTALLATION FOR RECLAMATION OF PROPELLANT CHARGES OF SMALL-SIZE ROCKET ENGINES

FIELD: rocketry. ^ SUBSTANCE: proposed installation contains accumulating reservoir, dust trap and adsorber, all connected with engine nozzle by gas lines and arranged in technological sequence. Dust trap is made in form of hermetically sealed chamber provided with upper and lower rows of plates arr...

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Bibliographische Detailangaben
Hauptverfasser:	KARMANOV N.N, SAKOV JU.L, KARIMOV V.Z, KARMANOV V.V, BURDJUGOV S.I, OPARIN V.G, SHCHERBAKOV JU.N, VAJSMAN JA.I
Format:	Patent
Sprache:	eng ; rus
Schlagworte:	BLASTING COMBUSTION APPARATUS COMBUSTION ENGINES COMBUSTION PROCESSES CONSUMING WASTE PRODUCTS BY COMBUSTION CREMATION FURNACES 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 installation contains accumulating reservoir, dust trap and adsorber, all connected with engine nozzle by gas lines and arranged in technological sequence. Dust trap is made in form of hermetically sealed chamber provided with upper and lower rows of plates arranged at tilting at equal angle. Plates of upper and lower rows alternate, and their outer edges overlap each other. Coarse and fine filters are installed between dust trap and adsorber. Said filters made in one housing are arranged on wire skeleton. Adsorber is made in form of vertical cylinder whose lower part is filled with crushed stone, and upper part, with activated charcoal. ^ EFFECT: provision of ecologically safe combustion of solid-propellant charges of small-size rocket engine in the air. ^ 4 dwg