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Injector design criteria using noncircular orifice geometryRocket engine propellant injectors with noncircular orifice geometry, presenting experimental spray patterns and predicted performance for noncircular and circular orifice configurations
Document ID
19710044823
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Clapp, S. D.
Mchale, R. M.
Nurick, W. H.
Date Acquired
August 6, 2013
Publication Date
April 1, 1971
Subject Category
Propulsion Systems
Accession Number
71A25520
Funding Number(s)
CONTRACT_GRANT: NAS9-9528
Distribution Limits
Public
Copyright
Other

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