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.
Vibroacoustic Analysis of Large Heat Rejection Radiators for Future Spacecraft
Spacecraft and Launch Vehicle Dynamic Environment Workshop ; 2005 ; El Segundo, CA, United States
2006-01-01
Aufsatz (Konferenz)
Keine Angabe
Englisch
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