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タイトルAcoustic Testing of the Cassini Spacecraft and Titan IV Payload Fairing
本文(外部サイト)http://hdl.handle.net/2060/19970026090
著者(英)McNelis, Anne M.; Hughes, William O.
著者所属(英)NASA Lewis Research Center
発行日1997-07-01
言語eng
内容記述A Cassini spacecraft simulator in a full scale 60 foot high Titan 4 payload fairing with various acoustic blanket designs and configurations was recently tested in a large reverberant acoustic chamber. A first part companion paper provides the test configuration details and other background information. This paper addresses the results obtained from this test program. Emphasis will be on the effects of the new blanket designs on reducing the payload fairing's internal acoustics and the vibration response of the spacecraft's Radioisotope Thermoelectric Generators. Other results discussed include: the effect of blankets on fairing vibration, the effect of partial blanket coverage on acoustics and vibration and the effect of tuned vibration absorbers.
NASA分類Spacecraft Design, Testing and Performance
レポートNO97N25439
NASA-TM-107475
NAS 1.15:107475
E-10764
権利No Copyright


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