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RQL Integrated Module Rig TestThis report documents the activities conducted under Work Breakdown Structure (WBS) 1.0.2.7 of the NASA Critical Components (CPC) Program to evaluate the low emissions potential of a Rich-Quench-Lean combustor capable of achieving the program goal of emissions of nitrogen oxides (NOxEI) less than 5 gm/Kg fuel at the supersonic light condition while maintaining combustion efficiencies in excess of 99.9 percent. The chosen combustor module would then be tested in the subscale annular rig test prior to testing in the subscale core engine demonstrator, if the RQL concept were to be chosen at the Combustor Downselect.
Document ID
20040033929
Acquisition Source
Headquarters
Document Type
Contractor Report (CR)
Authors
Koopman, Frederick S.
(Pratt and Whitney Aircraft Group West Palm Beach, FL, United States)
Ols, John T.
(Pratt and Whitney Aircraft Group West Palm Beach, FL, United States)
Padget, Frederick C., IV
(Pratt and Whitney Aircraft Group West Palm Beach, FL, United States)
Siskind, Kenneth S.
(Pratt and Whitney Aircraft Group West Palm Beach, FL, United States)
Holdeman, James D.
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
September 7, 2013
Publication Date
February 1, 2004
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA/CR-2004-212881
MTD211A5
E-14295
Report Number: NASA/CR-2004-212881
Report Number: MTD211A5
Report Number: E-14295
Funding Number(s)
WBS: WBS 22-714-01-39
CONTRACT_GRANT: NAS3-27235
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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