Specifi cation
The proposed vibration protection
is an autonomous passive system installed
between the upper stage of carrier rocket
and the spacecraft adapter. Its main element
is an elastic dissipative module.
One-dimensional motion of the vibroprotective
system along the longitudinal axis is ensured
by special guide rods
Advantages
The proposed system is lightweight
and compact and damps the longitudinal
vibrations in a wider frequency range
as compared with the known counterparts.
It reduces a longitudinal vibration load
on Sich-2M spacecraft over twice at a frequency
ranging from 5 to 10 Hz and 10 times
within the range from 10 to 100 Hz
Areas of Application
The system is to be used for reducing
vibration loads on the spacecraft
Stage of Development.
Suggestions for Commercialization
IRL2, TRL2
Principal diagram, sketch, and mathematical
model of system for spacecraft protection
from longitudinal vibration load during
its orbiting are proposed
IPR Protection
IÐ R1
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