2016
DOI: 10.1121/1.4953817
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Analysis and modeling of infrasound from a four-stage rocket launch

Abstract: Infrasound from a four-stage sounding rocket was recorded by several arrays within 100 km of the launch pad. Propagation modeling methods have been applied to the known trajectory to predict infrasonic signals at the ground in order to identify what information might be obtained from such observations. There is good agreement between modeled and observed back azimuths, and predicted arrival times for motor ignition signals match those observed. The signal due to the high-altitude stage ignition is found to be … Show more

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Cited by 11 publications
(15 citation statements)
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“…Out of the 60 planned infrasound arrays, currently 49 arrays are certified and sending data in real-time to the International Data Center in Vienna (status in September 2017). Observations of infrasound from rockets on the IMS infrasound arrays are routinely made as shown, for example, by and Blom et al (2016), as expected from the earlier studies.…”
Section: Introductionmentioning
confidence: 56%
“…Out of the 60 planned infrasound arrays, currently 49 arrays are certified and sending data in real-time to the International Data Center in Vienna (status in September 2017). Observations of infrasound from rockets on the IMS infrasound arrays are routinely made as shown, for example, by and Blom et al (2016), as expected from the earlier studies.…”
Section: Introductionmentioning
confidence: 56%
“…For the Space Shuttle, we observe impulsive signals from the solid fuel booster ignition (Blom et al., 2016; Olson, 2012) and ascent between 20:54 and 21:07 UTC, characterized by increasing apparent velocities from left to right, indicative of signal returns from increasing altitudes as time progresses (Pilger et al., 2020; Silber et al., 2018). These are preceded by a second group of signals following the booster separation and descent between 20:45 and 20:53 UTC and a third, weak signature probably from booster splashdown between 20:39 and 20:44 UTC.…”
Section: Resultsmentioning
confidence: 99%
“…Pilger et al 2021a ). The principal sources are aeroacoustic energy generated by supersonic engine exhaust and the Mach cone that forms when the rocket reaches supersonic velocities (Kaschak et al 1970 ; Cotten and Donn 1971 ; Blom et al 2016 ; McLaughlin et al 2000 ). Two distinct sets of signals are registered, where one group represents the sound from the direction of the launch site (Donn et al 1968 ; Balachandran and Donn 1971 ) and the other represents the sound originating from the re-entry of the first or second stage.…”
Section: Infrasonic Sourcesmentioning
confidence: 99%
“…Signals of a few (3 min; Kaschak et al 1970 ) to several minutes (~ 10 min) in length with gradually increasing and decreasing amplitudes (Balachandran and Donn 1971 ; McLaughlin et al 2000 ) have been detected, with the signal length correlating with the size of the re-entering objects and with burn time in the near field (Blom et al 2016 ). The signal shape changes from impulsive to more emergent with increase in distance (Evers et al 2018 ).…”
Section: Infrasonic Sourcesmentioning
confidence: 99%