|
RU2573695C1
|
|
Control over spacecraft at its ascent to earth artificial satellite orbit
|
|
RU2573509C1
|
|
Monitoring of asteroid-comet danger
|
|
RU2570009C1
|
|
Warning of danger in near-earth space and on earth and acs to this end
|
|
RU2552770C1
|
|
Control over spacecraft at descent in atmosphere with application of aerodynamic property
|
|
RU2568515C1
|
|
Band prepreg for fabrication of thermal-protective coating of pressure restraint layer of hypersonic re-entry aircraft housing
|
|
RU2568514C1
|
|
Immediate sealing of punched hole in manned spaceship body and device to this end
|
|
RU2561490C1
|
|
Control over spacecraft deorbit from earth artificial satellite orbit
|
|
RU2566322C1
|
|
Radio transmitter
|
|
RU2559392C1
|
|
Removal of non-functional spacecraft from geostationary orbit
|
|
RU2559616C1
|
|
Towed decoy target
|
|
RU2559401C1
|
|
Diagnostic of aircraft service systems operating conditions
|
|
RU2566171C2
|
|
Method for conflict resolution in spacecraft flight control
|
|
RU2561655C2
|
|
Space vehicle
|
|
RU2559430C2
|
|
Control over spacecraft descent from earth artificial satellite orbit
|
|
RU2559622C2
|
|
Clamping device to secure specimen during bend fatigue testing of flat specimens
|
|
RU2546025C1
|
|
Method of gas-dynamic action on dangerous space body and device for its implementation
|
|
RU2537192C1
|
|
Method of control over spacecraft descent in atmosphere of planets
|
|
RU2537193C1
|
|
Method of control over spacecraft descent in atmosphere of planets
|
|
RU2555590C2
|
|
Device for treating plant material
|
|
RU2544286C1
|
|
Spacecraft hardware passive protection against vibratory micro accelerations
|
