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Ground test program for new Atlas payload fairingsTo establish the competitiveness of the revitalized family of Atlas launch vehicles (I, II, IIA, and IIAS) a new series of payload fairings, an 11-foot and a 14-foot diameter version, were designed to accommodate the widest possible variety of satellites. Because these aluminum fairings are new designs, the plant at which they are produced is new, and launch customers are very anxious to fly their payloads, an ambitious and efficient test program is essential. Five major tests have been planned for completion within the span of one calendar year. One of these has been completed, with every indication that it was a success, one is currently under way, and two more are scheduled to start in the month of April. Through effective use of test assets, facilities, and personnel, all testing will be completed, allowing the fairing design to be completely characterized and then qualified through analysis prior to first launch of each of the fairings.
Document ID
19910001002
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Robbins, Michael J.
(General Dynamics Corp. San Diego, CA, United States)
Date Acquired
September 6, 2013
Publication Date
March 1, 1990
Publication Information
Publication: NASA, Langley Research Center, Research in Structures, Structural Dynamics and Materials, 1990
Subject Category
Structural Mechanics
Accession Number
91N10315
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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