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Investigation of Eight-stage Bleed-type Turbine for Hydrogen-propelled Nuclear Rocket Applications. II - Experimental Overall and Stage Group Performance Determined in Cold Nitrogen

Author
Rohlik, H. E.
Published
Mar 1, 1962.
Physical Description
1 electronic document
Online Version

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Unclassified, Unlimited, Publicly available.
Free-to-read Unrestricted online access
Summary
Eight-stage bleed-type turbine for hydrogen propelled nuclear rocket applications - experimental overall and stage group performance determined in cold nitrogen
Other Subject(s)
Collection
NASA Technical Reports Server (NTRS) Collection.
Note
Document ID: 19660030322.
Accession ID: 66N39612.
NASA-TM-X-481.
Terms of Use and Reproduction
No Copyright.
View MARC record | catkey: 15435900