One of the most severe environment that a satellite will be subjected to during its lifetime will occur during qualification testing and launch. This paper summarizes the results and status of research efforts in the area of satellite isolation from the launch environment. The objective of this effort was to reduce the launch induced-dynamic acceleration of the satellite by insertion of a passive isolator. Isolation issues involving the use of passive elements and launch vehicle system-level requirements will be discussed.
Passive Isolation Systems for Launch Vehicles
Fifth International Conference on Space ; 1996 ; Albuquerque, New Mexico, United States
1996-07-19
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Passive Isolation Systems for Launch Vehicles
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