Add to ORKGA flight propulsion system preliminary design was established that meets the program goals of at lea...
A brief review of the current NASA Energy Efficient Engine (E(3)) Project is presented. Included in ...
The preliminary operating specification, envelopes, and weight are presented for the selected engine...
The requirements imposed on the airbreathing engines by the shuttle mission and some results from en...
The Benefit/Cost Study portion of the NASA-sponsored Energy Efficient Engine Component Development a...
The status of NASA's Energy Efficient Engine Project, a comparative government-industry effort aimed...
This paper will present technologies and concepts for novel aeropropulsion systems. These technologi...
The advancement of technology in gas turbine engines used for aerospace propulsion has been focused ...
Design and systems considerations are presented on an engine concept selection for further prelimina...
The future orbit transfer vehicle (OTV) requirements which dictate the need for a highly versatile, ...
This study had the objectives of determining the most promising conventional and variable cycle engi...
The topics covered include the following: (1) Advanced Launch System (ALS); (2) life cycle cost/lb p...
The final design and analysis of the flight propulsion system is presented. This system is the conce...
In anticipation of an eventual VTOL requirement for civil aviation, NASA has been conducting studies...
The three engine programs that constitute the propulsion portion of NASA's Aircraft Energy Efficienc...
A flight propulsion system preliminary design was established that meets the program goals of at lea...
A brief review of the current NASA Energy Efficient Engine (E(3)) Project is presented. Included in ...
The preliminary operating specification, envelopes, and weight are presented for the selected engine...
The requirements imposed on the airbreathing engines by the shuttle mission and some results from en...
The Benefit/Cost Study portion of the NASA-sponsored Energy Efficient Engine Component Development a...
The status of NASA's Energy Efficient Engine Project, a comparative government-industry effort aimed...
This paper will present technologies and concepts for novel aeropropulsion systems. These technologi...
The advancement of technology in gas turbine engines used for aerospace propulsion has been focused ...
Design and systems considerations are presented on an engine concept selection for further prelimina...
The future orbit transfer vehicle (OTV) requirements which dictate the need for a highly versatile, ...
This study had the objectives of determining the most promising conventional and variable cycle engi...
The topics covered include the following: (1) Advanced Launch System (ALS); (2) life cycle cost/lb p...
The final design and analysis of the flight propulsion system is presented. This system is the conce...
In anticipation of an eventual VTOL requirement for civil aviation, NASA has been conducting studies...
The three engine programs that constitute the propulsion portion of NASA's Aircraft Energy Efficienc...
A flight propulsion system preliminary design was established that meets the program goals of at lea...
A brief review of the current NASA Energy Efficient Engine (E(3)) Project is presented. Included in ...
The preliminary operating specification, envelopes, and weight are presented for the selected engine...