|
RU2209495C1
|
|
Support-rotating device
|
|
RU2216491C1
|
|
Method of filling oxidizer tank of launch vehicle of aerospace system with liquid oxygen
|
|
RU2214551C1
|
|
Quick-release aggregate
|
|
RU2214550C1
|
|
Quick-release aggregate
|
|
RU2213611C1
|
|
Plant for decarbonization of solutions containing hydroxide of alkali metal
|
|
RU2216678C2
|
|
Quick-detachable unit
|
|
RU2216827C2
|
|
Procedure determining charging time of sealed metal- hydrogen storage battery
|
|
RU2216676C2
|
|
Quickly-detachable unit
|
|
RU2216677C2
|
|
Quick-detachable unit
|
|
RU2214198C1
|
|
Artificial ankle joint
|
|
RU2216653C2
|
|
Hydraulic drive adjusting method
|
|
RU2215901C2
|
|
Adsorption pump
|
|
RU2215900C2
|
|
Adsorption pump
|
|
RU2214351C2
|
|
Descent vehicle with load-bearing case and method of landing such vehicle
|
|
RU2213682C2
|
|
Spacecraft for descent in atmosphere of planet and method of its descent (variants)
|
|
RU2211417C1
|
|
Continuous-belt drier
|
|
RU2209155C1
|
|
Method of assembly of nose unit on adapter of launch vehicle (variants) and device for realization of this method
|
|
RU2208560C1
|
|
On-board complex of cargo spacecraft
|
|
RU2213635C2
|
|
Method for degassing articles
|
|
RU2208559C1
|
|
Method of determination of inertial characteristics of spacecraft in the course of control by means of powered gyroscopes and jet engines
|
