RU2396706C1
|
|
Power key on mis transistor
|
RU2369851C1
|
|
Impact testing stand
|
RU2383000C2
|
|
Method of space vehicle tests for mechanical action
|
RU2367903C1
|
|
Device for measurement of angular displacements
|
RU2358383C1
|
|
Mis transistor power key
|
RU2366915C1
|
|
Method for testing of spacecraft equipment by mechanical actions
|
RU2369538C1
|
|
Volume compensator for spacecraft liquid temperature control system
|
RU2384491C2
|
|
Spacecraft thermoregulating system
|
RU2366914C1
|
|
Method for testing of spacecraft structural elements, in particular honeycomb panels, by mechanical actions
|
RU2367920C1
|
|
Method for detection of tank own frequencies
|
RU2371360C2
|
|
Device to connect/disconnect structural elements
|
RU2360223C1
|
|
Method of testing mechanical effects on spacecraft equipment
|
RU2369537C2
|
|
Method of assembling spacecraft
|
RU2369536C2
|
|
Spacecraft temperature control system
|
RU2355106C1
|
|
Converter of shaft rotation angle into code
|
RU2362712C1
|
|
Space vehicle temperature control system
|
RU2362711C1
|
|
Space vehicle temperature control system
|
RU2344524C1
|
|
Method of large reflector manufacturing
|
RU2354948C1
|
|
Method of testing spacecraft under vibro-acoustic effect
|
RU2354950C1
|
|
Method of testing impact effects on spacecraft
|