One drawback to the ability to land boosters of orbital launch vehicles, such as the Falcon 9, is the associated reentry sonic boom. Because of the Falcon 9 booster shape and landing orientation, the observed waveform at the ground contains three shocks (a triple boom), rather than the two associated with a traditional N-wave. To assess the impact of these sonic booms, acoustic data from a Falcon-9 booster landing at Vandenberg Space Force Base are analyzed. The data were collected in Lompoc, CA, at locations 7-14 km away from the landing site. Waveform and spectral characteristics are examined and various metrics, including A-weighted Sound Exposure Levels (ASEL), are calculated. These metrics from the reentry sonic booms are compared with metrics calculated from the launch noise.
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April 2022
Meeting abstract. No PDF available.
April 01 2022
Analysis of sonic booms from Falcon 9 booster landings Free
J T. Durrant;
J T. Durrant
Dept. of Phys. and Astronomy, Brigham Young Univ., N283 ESC, Provo, UT 84602, [email protected]
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Kent L. Gee;
Kent L. Gee
Dept. of Phys. and Astronomy, Brigham Young Univ., Provo, UT
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Logan T. Mathews;
Logan T. Mathews
Phys. and Astronomy, Brigham Young Univ., Provo, UT
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Grant W. Hart
Grant W. Hart
Dept. of Phys. and Astronomy, Brigham Young Univ., Provo, UT
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J T. Durrant
Kent L. Gee
Mark C. Anderson
Logan T. Mathews
Grant W. Hart
Dept. of Phys. and Astronomy, Brigham Young Univ., N283 ESC, Provo, UT 84602, [email protected]
J. Acoust. Soc. Am. 151, A86 (2022)
Connected Content
A companion article has been published:
Initial comparison of a Falcon-9 reentry sonic boom with other launch-related noise
Citation
J T. Durrant, Kent L. Gee, Mark C. Anderson, Logan T. Mathews, Grant W. Hart; Analysis of sonic booms from Falcon 9 booster landings. J. Acoust. Soc. Am. 1 April 2022; 151 (4_Supplement): A86. https://doi.org/10.1121/10.0010743
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