Add to ORKGThe technology that will improve the energy efficiency of propulsion systems for subsonic commercial aircraft is investigated. A reduction of 14.4% in cruise installed sfc (0.572 versus 0.668 for the CF6-50C) and a direct operation cost reduction in excess of the 5% goal is projected. Noise and emissions projections are consistent with the established goals
Propulsion system characteristics for a long range, high subsonic (Mach 0.90 - 0.98), jet commercial...
The NASA Fundamental Aeronautics Program Subsonic Fixed Wing Project and Integrated Systems Research...
A brief review of the current NASA Energy Efficient Engine (E(3)) Project is presented. Included in ...
The development of the technology to improve energy efficiency of propulsion systems for subsonic co...
Technology for achieving lower installed fuel consumption and lower operating costs in future commer...
Results of aircraft/engine integration studies conducted on an advanced flight propulsion system are...
A flight propulsion system preliminary design was established that meets the program goals of at lea...
The three engine programs that constitute the propulsion portion of NASA's Aircraft Energy Efficienc...
The status of NASA's Energy Efficient Engine Project, a comparative government-industry effort aimed...
The characteristics of an advanced Flight Propulsion System (FPS) suitable for introduction in the l...
As part of the NASA-sponsored Engine Component Improvement (ECI) Program, a feasibility analysis of ...
The Energy Efficient Engine Project is directed at providing, by 1984, the advanced technologies whi...
The preliminary design of General Electric's Energy Efficient Engine (E3) was reported in detail in ...
Parametric design and mission evaluations of advanced turbofan configurations were conducted for fut...
The Benefit/Cost Study portion of the NASA-sponsored Energy Efficient Engine Component Development a...
Propulsion system characteristics for a long range, high subsonic (Mach 0.90 - 0.98), jet commercial...
The NASA Fundamental Aeronautics Program Subsonic Fixed Wing Project and Integrated Systems Research...
A brief review of the current NASA Energy Efficient Engine (E(3)) Project is presented. Included in ...
The development of the technology to improve energy efficiency of propulsion systems for subsonic co...
Technology for achieving lower installed fuel consumption and lower operating costs in future commer...
Results of aircraft/engine integration studies conducted on an advanced flight propulsion system are...
A flight propulsion system preliminary design was established that meets the program goals of at lea...
The three engine programs that constitute the propulsion portion of NASA's Aircraft Energy Efficienc...
The status of NASA's Energy Efficient Engine Project, a comparative government-industry effort aimed...
The characteristics of an advanced Flight Propulsion System (FPS) suitable for introduction in the l...
As part of the NASA-sponsored Engine Component Improvement (ECI) Program, a feasibility analysis of ...
The Energy Efficient Engine Project is directed at providing, by 1984, the advanced technologies whi...
The preliminary design of General Electric's Energy Efficient Engine (E3) was reported in detail in ...
Parametric design and mission evaluations of advanced turbofan configurations were conducted for fut...
The Benefit/Cost Study portion of the NASA-sponsored Energy Efficient Engine Component Development a...
Propulsion system characteristics for a long range, high subsonic (Mach 0.90 - 0.98), jet commercial...
The NASA Fundamental Aeronautics Program Subsonic Fixed Wing Project and Integrated Systems Research...
A brief review of the current NASA Energy Efficient Engine (E(3)) Project is presented. Included in ...