|
RU2476920C1
|
|
Multi-task aircraft control data system
|
|
RU2472956C2
|
|
Supersonic controlled air intake
|
|
RU2460892C1
|
|
Method of adjusting supersonic air intake
|
|
RU2460982C1
|
|
Method of determining aerodynamic characteristics of aircraft
|
|
RU2462395C2
|
|
Airframe of multipurpose class vi aircraft
|
|
RU2440916C1
|
|
Aircraft in integral aerodynamic configuration
|
|
RU2425318C2
|
|
Device (adapter) to item for angle gauge
|
|
RU2400402C1
|
|
Multimode high maneuverability aircraft of integral aerodynamic configuration
|
|
RU2478528C2
|
|
Method of defining target fuel residue in slipper fuel tank in fueling
|
|
RU2478529C2
|
|
Method of reducing signature of jet engine (versions)
|
|
RU2392586C1
|
|
Aircraft information-control system
|
|
RU2376210C1
|
|
System and method for aircraftfuel-tank pressurisation by neutral gas
|
|
RU2367881C1
|
|
Armored structure
|
|
RU2356800C1
|
|
Airplane fuel system
|
|
RU2367979C2
|
|
Semiconductor small-size coordinate detector of x-ray (radiation induced) emission
|
|
RU2341775C1
|
|
Method of determining aircraft aerodynamic angle
|
|
RU2352913C1
|
|
Method of defining gas turbine gas-dynamic stability margin
|
|
RU2326791C1
|
|
Hardware liquid cooling system
|
|
RU2327608C1
|
|
System of recovering aircraft from spin
|
|
RU2327616C1
|
|
Device for mounting-dismantling and transportation of flight vehicle nose cone
|
