UNIT FOR HYDROCARBON ROCKET FUEL RESEARCH Russian patent published in 2018 - IPC G01N33/22 

Abstract RU 2664443 C1

FIELD: monitoring and measurement equipment.

SUBSTANCE: invention relates to test and measurement equipment. Unit comprises a closed hydraulic circuit including a fuel tank, pressure pump with a pneumatic drive, pneumohydraulic accumulator installed after the pump, heat-insulated working section, heat exchanger-cooler installed after the working section and in front of the fuel tank, and a heater that is a constant current source with current and voltage meters and with power buses connected to the ends of the working section. Unit also includes sensors for temperature, pressure and fuel consumption in the circuit.

EFFECT: higher accuracy of determining the performance characteristics of hydrocarbon rocket fuel is achieved by creating conditions in an experiment close to real.

1 cl, 1 dwg

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RU 2 664 443 C1

Authors

Danilov Vasilij Viktorovich

Zubkov Nikolaj Anatolevich

Velikanov Aleksandr Anatolevich

Lukoyanov Yurij Mikhajlovich

Sobolev Viktor Vladimirovich

Maklakov Nikolaj Nikolaevich

Dates

2018-08-17Published

2018-02-09Filed