RU2392595C1
|
|
Tightness control method
|
RU2390480C1
|
|
Spacecraft blind cover flap
|
RU2393651C1
|
|
Device for metallisation of movable elements of structure
|
RU2391264C1
|
|
Spacecraft light protection device
|
RU2399122C1
|
|
Method for operation of nickel-hydrogen accumulator batteries of spacecraft power supply system
|
RU2389661C1
|
|
Device to discharge liquid oxygen vapors from carrier rocket side block oxidiser tank
|
RU2387915C1
|
|
Quick disconnect
|
RU2382454C1
|
|
Method for transmission of measurement signal via current collector and device for its realisation
|
RU2381123C1
|
|
Car bogie axle box damper
|
RU2380714C1
|
|
Method for processing of strain sensor signal and device for its realisation
|
RU2368542C1
|
|
Space-mission rocket
|
RU2366852C1
|
|
Self-locking hydraulic connector
|
RU2369534C1
|
|
Device for dividing nose fairing halves
|
RU2349518C1
|
|
Space vehicle power supply system simulation stand
|
RU2375269C2
|
|
Method of spacecraft orientation and device to this end
|
RU2355583C2
|
|
Production method of large three-layer structures from polymer composites
|
RU2348507C1
|
|
All-purpose hydraulically-driven suspended tongs
|
RU2345931C1
|
|
Detachable tail section of carrier rocket
|
RU2344334C1
|
|
Quick-split joint of pipelines
|
RU2331553C1
|
|
Thermoregulating coating of "sollar reflector" type
|