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Analyses of Noise from Reusable Solid Rocket Motor (RSRM) FiringsNASA s Space Launch Vehicle (SLS) program has chosen the Reusable Solid Rocket Motor V (RSRMV) as the booster system for initial flights. Lift off acoustics continue to be a consideration in overall vehicle vibroacoustic evaluations and launch pad modifications. Work started with the Ares program to understand solid rocket noise mechanisms is continuing through SLS program in conjunction with BYU/Blue Ridge Research Consulting.
Document ID
20130000695
Acquisition Source
Marshall Space Flight Center
Document Type
Presentation
Authors
Gee, Kent L. (Brigham Young Univ. Provo, UT, United States)
Kenny, R. Jeremy (NASA Marshall Space Flight Center Huntsville, AL, United States)
Jerome, Trevor W. (Brigham Young Univ. Provo, UT, United States)
Neilsen, Tracianne B. (Brigham Young Univ. Provo, UT, United States)
Hobbs, Christopher M. (Wyle Labs., Inc. Huntsville, AL, United States)
James, Michael M. (Blue Ridge Research and Consulting , LLC Asheville, NC, United States)
Date Acquired
August 27, 2013
Publication Date
October 22, 2012
Subject Category
Acoustics
Report/Patent Number
M12-2219
Report Number: M12-2219
Meeting Information
Meeting: 164th Meeting of the Acoustical Society of America
Location: Arlington, VA
Country: United States
Start Date: October 22, 2012
End Date: October 26, 2012
Distribution Limits
Public
Copyright
Public Use Permitted.

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