RU2635758C1
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System for controlling supersonic ramjet engine
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RU2634661C1
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Ball bearing
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RU2635757C1
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Method of control of ramjet engine of winged rocket
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RU2635595C1
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METHOD OF PRODUCING PARTS FOR GAS TURBINE ENGINES MADE OF TITANIUM PSEUDO-β-NICKEL ALLOY WITH Ti-Al-Mo-V-Cr-Fe MASTER ALLOY
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RU2630346C1
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Ball bearing
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RU2635704C1
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Device for connection and disconnection of air vehicle separated stages electrical connections
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RU2627991C1
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Object angle sensor
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RU2624447C1
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Method of controlling autonomous power supply system of spacecraft
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RU2642471C1
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Casing shell of aircraft
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RU2637166C1
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Device for cylinder gas charging and sealing under pressure
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RU2623592C1
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Rotary gas turbine engine
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RU2617903C1
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Method for using fuel from aircraft tank
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RU2622181C1
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Thermal protection of unsealed compartments of aircraft powerplant
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RU2630347C1
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Method of preparing rocket fuel components for refueling rocket propulsion systems
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RU2630858C1
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Device for connection and disconnection of electric couplings of separated aircraft stages
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RU2622173C1
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Method of ensuring thermal regime of the instrument compartment of aircraft
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RU2618572C1
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Method of fixing window flat protective glass
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RU2628410C1
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Single wire termination method with electrical connector contact by crimping method
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RU2615028C1
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Method of unmanned aerial vehicles longitudinal angular motion stability signal forming
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RU2629138C1
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Manufacture method of compressor blades from titanium alloy vt6
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