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Cassini Environmental Test and Analysis Program SummaryThis paper presents an overview of the Cassini Project's environmental test and analysis program during thc spacecraft development phase - October 1989 to launch on October 1997. It describes the program's objectives and requirements, summarizes the approach used to achieve them, and provides the margins that were achieved in the final design. Assembly and system level environmental tests that were performed included dynamic, thermal, electromagnetic compatibility (EMC), and magnetic tests. Analysis was used to verify that the environmental requirements of radiation, solid particles including micrometeoroids, and single event effects have been satisfied. The environmental program implemented on Cassini satisfied the spirit and intent of the requirements imposed by the Project during the spacecraft's development. The lessons learned from the Cassini environmental program are discussed.
Document ID
20000034968
Acquisition Source
Jet Propulsion Laboratory
Document Type
Conference Paper
External Source(s)
Authors
Hoffman, Alan R.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA United States)
Forgrave, John C.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA United States)
Date Acquired
August 19, 2013
Publication Date
March 16, 1999
Publication Information
Publisher: Institute of Environmental Sciences and Technology
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
No Number:
Distribution Limits
Public
Copyright
Other

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