SOLID-PROPELLANT ROCKET ENGINE TEST SET

FIELD: rocketry; test facilities. ^ SUBSTANCE: proposed test set designed for testing small-size solid propellant rocket engines contains storage reservoir and combustion products cleaning system interconnected by gas-dynamic duct. Storage reservoir is installed directly after engine and is hermetic...

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Bibliographische Detailangaben
Hauptverfasser:	KARMANOV N.N, SAKOV JU.L, KARIMOV V.Z, BURDJUGOV S.I, KHALTURIN V.G, 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; test facilities. ^ SUBSTANCE: proposed test set designed for testing small-size solid propellant rocket engines contains storage reservoir and combustion products cleaning system interconnected by gas-dynamic duct. Storage reservoir is installed directly after engine and is hermetically connected with engine nozzle. Gas cooler is installed in gas-dynamic duct between storage reservoir and cleaning system. ^ EFFECT: no adverse action on environment at combustion of solid propellant charge in the open. ^ 1 dwg