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The effect of several injector face baffle configurations on screech in a 20,000-pound thrust hydrogen-oxygen rocket

Author
Scott, H. E.
Published
Jan 1, 1966.
Physical Description
1 electronic document
Additional Creators
Hannum, N. P.
Online Version

Availability

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Restrictions on Access
Unclassified, Unlimited, Publicly available.
Free-to-read Unrestricted online access
Summary
Effects of injector face baffle configurations on screech in hydrogen-oxygen rocket engine
Other Subject(s)
Collection
NASA Technical Reports Server (NTRS) Collection.
Note
Document ID: 19670002005.
Accession ID: 67N11334.
NASA-TM-X-52251.
Terms of Use and Reproduction
No Copyright.
View MARC record | catkey: 15957532