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Staged Turbojet Engine Would Emit Less NONew turbojet-engine concept could reduce nitric oxide emissions to a level from one-fifteenth to as little as one three-hundredth that of conventional units. Multiple-stage combustor could overcome flame instability problems associated with previous low-flame-temperature systems. It operates in a relatively-simple adiabatic mode without elaborate fuel-flow and air circulation patterns.,
Document ID
19810000213
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Craig, R. A.
(Centre for Research in Experimental Space Science, York University)
Pritchard, H. O.
Date Acquired
August 11, 2013
Publication Date
November 1, 1982
Publication Information
Publication: NASA Tech Briefs
Volume: 6
Issue: 2
ISSN: 0145-319X
Subject Category
Machinery
Report/Patent Number
ARC-10814
Accession Number
81B10213
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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