New 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.,
Staged Turbojet Engine Would Emit Less NO
NASA Tech Briefs ; 6 , 2
1982-11-01
Sonstige
Keine Angabe
Englisch
Fast engine model for FMU-less small turbojet engines
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