RU2581274C2
|
|
Modular spacecraft
|
RU2549523C1
|
|
Method for mutation testing of radio-electronic equipment and control software thereof
|
RU2583863C2
|
|
Folding parabolic reflector and method of making same
|
RU2549123C1
|
|
Matrix command generator
|
RU2538301C1
|
|
Half bridge galvanic isolated pulse-power amplifier
|
RU2540785C1
|
|
Bridge self-maintained voltage transducer
|
RU2549831C1
|
|
Accumulator storage battery of space vehicle
|
RU2550079C2
|
|
Method of load feeding by direct current in autonomous electric power supply system of man-made satellite
|
RU2542883C1
|
|
Device for monitoring and undermining sequential chains of pyrocartridges
|
RU2549545C2
|
|
Digital ferroprobe magnetometer
|
RU2564053C2
|
|
Measuring method of thermal fields of electric radio items
|
RU2549582C2
|
|
Ballistic support of spacecraft flight
|
RU2539710C1
|
|
Device to fix and separate parts of structure
|
RU2548314C2
|
|
Rotation system of double-wing solar panels
|
RU2530195C1
|
|
Sealing unit for detachable joint junction
|
RU2548590C2
|
|
Gas mass detector
|
RU2551442C2
|
|
Method of manufacturing of hp metal-plastic bottle
|
RU2524854C1
|
|
Device for detecting and correcting errors in parallel highway
|
RU2548664C2
|
|
Method of load feeding by direct current in autonomous electric power supply system of man-made satellite
|
RU2543079C2
|
|
Load power supply method by direct current
|