|
RU2556460C1
|
|
Control over drone mid-flight engine (versions) and device to this end
|
|
RU2583868C2
|
|
Method of target capture by laser homing head of unmanned aerial vehicle
|
|
RU2550100C1
|
|
Method for control of triggering altitude of warhead of unmanned airborne vehicle and device for its implementation
|
|
RU2541995C1
|
|
Method to receive signal of rocket separation from carrier and device to this end
|
|
RU2522787C1
|
|
Device of fixing in fold position of wing panels of unmanned aerial vehicle
|
|
RU2527967C1
|
|
Rocket magnetic safety device
|
|
RU2549044C2
|
|
Folding steering surface of airborne hitting means with spring-type unfolding drive
|
|
RU2513080C1
|
|
Compact aircraft wing rotary assembly
|
|
RU2533632C2
|
|
General-purpose analyser of digital interfaces of armament systems, and method for its manufacture
|
|
RU2499747C1
|
|
Drone compact air intake
|
|
RU2499746C1
|
|
Aircraft compact air intake
|
|
RU2502078C1
|
|
Method to check communication lines of carrier equipment and device for its realisation
|
|
RU2492413C1
|
|
Drop head fairing of aircraft (versions)
|
|
RU2481551C1
|
|
Compact single-operation safety device
|
|
RU2481676C1
|
|
Thermal battery with device of protection against electromagnetic radiation
|
|
RU2471585C1
|
|
Method of making thin-wall asymmetric bicurvature shells with flange
|
|
RU2489674C2
|
|
Compact controlled ammunition
|
|
RU2463210C1
|
|
Aircraft outer wing deployment and fixation device
|
|
RU2440607C1
|
|
Device for imitating carrier apparatus for controlling information exchange with rocket
|
|
RU2478061C2
|
|
Drone unified bearing module
|
