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Fundamental problems of injector design.Liquid propellant injector design for rocket thrust chambers, discussing mass and mixture ratio regulation
Document ID
19690054010
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Harrje, D. T.
Date Acquired
August 5, 2013
Publication Date
January 1, 1968
Publication Information
Publisher: TECHNIVISION SERVICES AND CIRCA PUBLICATIONS, INC.,
Subject Category
Propulsion Systems
Accession Number
69A31999
Funding Number(s)
CONTRACT_GRANT: NASR-217
Distribution Limits
Public
Copyright
Other

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