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Accession Number:
ADA361679
Title:
Whole Spacecraft Vibration Isolation.
Descriptive Note:
Master's thesis,
Corporate Author:
AIR FORCE INST OF TECH WRIGHT-PATTERSONAFB OH SCHOOL OF ENGINEERING
Report Date:
1999-03-01
Pagination or Media Count:
169.0
Abstract:
The Department of Defense identified launch vibration isolation as a major research interest. Reducing the loads a satellite experiences during launch will greatly enhance the reliability, lifetime, and payload to structure ratio. DoD satellite programs stand to benefit significantly from advances in vibration isolation technology.
Distribution Statement:
APPROVED FOR PUBLIC RELEASE