FIELD: mechanical engineering.
SUBSTANCE: invention relates to machine building. Stand for power plants testing contains propellants feed system with control units and process gas supply system, at that, on the output of the power plant a conduit connected to gas holder is installed, gas holder is connected to the compressor, which in turn is connected to the high-pressure cylinders system, gas holder is set on a moving platform, the cavity of supply tank gas pressurization with a propellant is connected to the compressor inlet, and the compressor outlet is connected to the gas inlet into the high-pressure cylinders.
EFFECT: invention can be used in testing of liquid rocket engines (LRE), and other power plants.
4 cl, 2 dwg
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