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    Vibroacoustic Analysis of Large Heat Rejection Radiators for Future Spacecraft (2006)
    In:  CASI
    Details
    Publication Date: 2019-07-13
    Description: Spacecraft structures such as antennas, solar arrays and radiator panels significantly respond to high acoustic levels seen at lift-off. Some future spacecraft may utilize nuclear electric propulsion that require large radiator panels to reject waste heat. A vibroacoustic assessment was performed for two different radiator panel designs. Results from the analysis of the two designs using different analytical approaches are presented and discussed.
    Keywords: Acoustics
    Type: Spacecraft and Launch Vehicle Dynamic Environment Workshop; Jun 21, 2005 - Jun 23, 2005; El Segundo, CA; United States
    Format: application/pdf
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