SOLID-PROPELLANT ROCKET ENGINE TEST SET Russian patent published in 2005 - IPC

Abstract RU 2267025 C2

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

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RU 2 267 025 C2

Authors

Burdjugov S.I.

Sakov Ju.L.

Karimov V.Z.

Karmanov N.N.

Vajsman Ja.I.

Khalturin V.G.

Dates

2005-12-27—Published

2004-01-05—Filed