RU2211349C1
|
|
Cartridge pressure accumulator
|
RU2215170C1
|
|
Mockup engine for determining burning rate of rocket solid propellant
|
RU2215169C1
|
|
Solid-propellant charge combustion method
|
RU2212395C1
|
|
Method of manufacturing mixed rocket fuel charges
|
RU2201520C1
|
|
Model engine for determining burning rate of solid propellant in stressed-deformed state
|
RU2208463C1
|
|
Flameless fire-extinguishing aerosol generator
|
RU2203871C1
|
|
Technology of manufacture of charges of blended solid propellant with predicted characteristics
|
RU2194687C1
|
|
Method for industrial production of mixed solid rocket fuel
|
RU2194945C1
|
|
Method for milling of fire-hazardous and dangerously explosive materials
|
RU2189840C1
|
|
Fire-suppressing aerosol generator
|
RU2188963C1
|
|
Installation for determination of burning rate of solid propellant in stressed- deformed state
|
RU2192554C1
|
|
Charge connected with solid propellant rocket engine body
|
RU2179743C1
|
|
Modulation flame detector
|
RU2194874C2
|
|
Plant for determining burning rate of solid propellant
|
RU2185396C1
|
|
Plasticized nitrocellulose production process
|
RU2174619C1
|
|
Casing of solid-propellant rocket engine, type "cocoon"
|
RU2194238C2
|
|
Fireworks rocket
|
RU2167327C1
|
|
Plant for determination of rate of burning of solid rocket propellant
|
RU2179703C1
|
|
Device for solid propellant temperature control of loaded charges of solid propellant
|
RU2170837C1
|
|
Charge forming method for solid-propellant rocket engine
|