Actions for High Pressure Regenerative Turbine Engine : 21st Century Propulsion

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High Pressure Regenerative Turbine Engine : 21st Century Propulsion

Author
Laganelli, A. L.
Published
March 2001.
Physical Description
1 electronic document
Additional Creators
Senick, Paul and Lear, W. E.
Online Version

Availability

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Restrictions on Access
Unclassified, Unlimited, Publicly available.
Free-to-read Unrestricted online access
Summary
A novel semi-closed cycle gas turbine engine was demonstrated and was found to meet the program goals. The proof-of-principle test of the High Pressure Regenerative Turbine Engine produced data that agreed well with models, enabling more confidence in designing future prototypes based on this concept. Emission levels were significantly reduced as predicted as a natural attribute of this power cycle. Engine testing over a portion of the operating range allowed verification of predicted power increases compared to the baseline.
Other Subject(s)
Collection
NASA Technical Reports Server (NTRS) Collection.
Note
Document ID: 20010026758.
NASA/CR-2001-210675.
GDL99-3.
E-12602.
NAS 1.26:210675.
Terms of Use and Reproduction
No Copyright.
View MARC record | catkey: 15423313