RU2533592C1
|
|
Spacecraft power plant fuel feed system
|
RU2521078C1
|
|
Transfer compartment of space mission vehicle assembly-protective unit
|
RU2520792C1
|
|
Valve
|
RU2521431C1
|
|
Drain-safety valve of oxidiser tank
|
RU2518016C1
|
|
Stamping unit for corrugated article production
|
RU2514015C1
|
|
Spacecraft light protection device cover assembly
|
RU2518137C2
|
|
Pulse-free device for unlocking of spacecraft moving elements
|
RU2497727C1
|
|
Spacecraft head servicing hatch
|
RU2522763C2
|
|
Spacecraft fuel tank for liquid components storing and delivery
|
RU2492384C1
|
|
Drain safety valve
|
RU2496045C1
|
|
Detachable joint
|
RU2509977C1
|
|
Self-aligning internal callipers
|
RU2504730C1
|
|
Method of control over integrity of current conducting coat on dielectric material
|
RU2503048C1
|
|
Space telescope supporting girder
|
RU2497732C1
|
|
Device for separation of rocket unit tail compartment
|
RU2496102C1
|
|
Laser vibration transducer
|
RU2493056C1
|
|
Earth remote sounding spacecraft
|
RU2489331C1
|
|
Space apparatus separation devices test bench
|
RU2492584C1
|
|
Optical-electronic converter
|
RU2488857C1
|
|
Hermetically sealed fibre-optic connector
|