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The separation test in vacuum of the Ariane 4 payload fairingThe separation tests performed during the qualification test program of the Ariane 4 Payload Fairing are described. This is the first fairing structure to be developed using carbon fiber technology. Two separation tests were performed under vacuum conditions. The primary objectives of these tests were to verify compliance with the vehicle imposed requirements and to establish the behavioral characteristics of the fairing structure itself.
Document ID
19890003241
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Butcher, J. R.
(Contraves Corp. Zurich, Switzerland)
Date Acquired
September 5, 2013
Publication Date
January 1, 1988
Publication Information
Publication: NASA, Goddard Space Flight Center, 15th Space Simulation Conference: Support the Highway to Space Through Testing
Subject Category
Launch Vehicles And Space Vehicles
Accession Number
89N12612
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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