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Mechanical suppression: Modern technology applied to an old artVarious suppressor configurations were analyzed and evaluated in an effort to reduce combustion instability and improved ballistic reproducibility of the MK 12 motor. A static firing test series of eight field return boosters featured two baseline motor firings with the existing suppressor in each motor, followed by two tests each of two different prototype suppressor designs. Results were analyzed and used to generate the design for the final two firings. Acoustic pressure pulsers were utilized to measure the damping effectiveness of the final design. The reduction in motor vibration and acoustic pressure levels between the baseline tests and the final two improved lightweight tests was significant. The average acceleration level of the motors equipped with flightweight rods was reduced to only 5% of the level in the unmodified motors; the average acoustic pressure level was reduced to 20%; maximum values were reduced to 6% for acceleration and 23% for pressure.
Document ID
19810007756
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Crockford, W. H.
(Naval Ordnance Station Indian Head, MD, United States)
Durney, T. E.
(Naval Ordnance Station Indian Head, MD, United States)
Scott, D. E.
(Naval Ordnance Station Indian Head, MD, United States)
Condon, J. A.
(Naval Ordnance Station Indian Head, MD, United States)
Date Acquired
August 11, 2013
Publication Date
November 1, 1980
Publication Information
Publication: NASA. Langley Research Center The 17th JANNAF Combust. Meeting, Vol. 1
Subject Category
Propellants And Fuels
Accession Number
81N16272
Funding Number(s)
CONTRACT_GRANT: N00174-77-C-1282
Distribution Limits
Public
Copyright
Other

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