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Acoustic Model Testing ChronologyScale models have been used for decades to replicate liftoff environments and in particular acoustics for launch vehicles. It is assumed, and analyses supports, that the key characteristics of noise generation, propagation, and measurement can be scaled. Over time significant insight was gained not just towards understanding the effects of thruster details, pad geometry, and sound mitigation but also to the physical processes involved. An overview of a selected set of scale model tests are compiled here to illustrate the variety of configurations that have been tested and the fundamental knowledge gained. The selected scale model tests are presented chronologically.
Document ID
20170008167
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Nesman, Tom
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
August 31, 2017
Publication Date
June 20, 2017
Subject Category
Launch Vehicles And Launch Operations
Acoustics
Report/Patent Number
M17-6086
Report Number: M17-6086
Meeting Information
Meeting: Spacecraft and Launch Vehicle Dynamic Environments Workshop
Location: El Segundo, CA
Country: United States
Start Date: June 20, 2017
End Date: June 22, 2017
Sponsors: NASA Headquarters
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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