Why does the Falcon-9 booster make a triple sonic boom during flyback? An initial analysis

When the SpaceX Falcon-9 rocket booster descends through the atmosphere after a launch, it produces a sonic boom with three shocks in the far field, rather than the usual two-shock N-wave. In this Letter, the additional shock's origin is explained using sonic boom theory, nonlinear propagation modeling, computational fluid dynamics, and photographic evidence. The extra central shock results from a forward-migrating compression wave caused by the grid fins merging with a rearward-migrating rarefaction wave caused by the lower portions of the booster, including the folded landing legs.

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Publication Details

Journal
JASA Express Letters
Published
2025-02-01
DOI
https://doi.org/10.1121/10.0035649
Citations
1
Primary Topic
Computational Fluid Dynamics and Aerodynamics
Type
article
Field-Weighted Citation Impact
1.33

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article

Why does the Falcon-9 booster make a triple sonic boom during flyback? An initial analysis

Kent L. Gee, Mark C. Anderson
1 citations
JASA Express Letters
Computational Fluid Dynamics and Aerodynamics
1.33
article

Why does the Falcon-9 booster make a triple sonic boom during flyback? An initial analysis

Kent L. Gee, Mark C. Anderson
article en
1 citations

Abstract

When the SpaceX Falcon-9 rocket booster descends through the atmosphere after a launch, it produces a sonic boom with three shocks in the far field, rather than the usual two-shock N-wave. In this Letter, the additional shock's origin is explained using sonic boom theory, nonlinear propagation modeling, computational fluid dynamics, and photographic evidence. The extra central shock results from a forward-migrating compression wave caused by the grid fins merging with a rearward-migrating rarefaction wave caused by the lower portions of the booster, including the folded landing legs.

JASA Express LettersVol. 5(2)
Brigham Young University (US)
Oak Ridge Institute for Science and Education
Openalex Percentile: Top 27%
Computational Fluid Dynamics and Aerodynamics
1.33
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