The NASA Aeronautics Research Mission Directorate (ARMD) Strategic Implementation Plan details an ambitious plan for aeronautical research for the next quarter century and beyond. It includes a number of advanced technologies needed to address requirements of the overall aviation community (domestic and international), with an emphasis on safety, efficiency, operational flexibility, and alternative propulsion air transport options. The six ARMD Strategic Thrust Areas (STAs) represent a specific set of multi-decade research agendas for creating the global aviation improvements most in demand by the aviation service consumers and the general public. To provide NASA with a measurement of the preeminent value of these research areas, it was nec...
The Commercial Aero-Propulsion Control Working Group (CAPCWG), consisting of propulsion control tech...
Specific to the application of any technology to a vehicle, such as circulation control, it is impor...
Propulsion requirements were determined for 0.5 and 0.7 Mach aircraft. Sensitivity studies were cond...
In the past few years, NASA (National Aeronautics and Space Administration) Aeronautics Research Mis...
This is a quick presentation on the UAM Research Visions which include the Commerical Operating Envi...
The Aeronautics Test Program (ATP) within the National Aeronautics and Space Administration (NASA) A...
This presentation educates public and stakeholders on NASA organization, ARMD programs and projects,...
The Overarching Mission of NASA's Aeronautics Research Mission Directorate (ARMD) is: To advance U.S...
The NASA Aeronautics Research Mission Directorate (ARMD) is bringing together public, private, and a...
This report is intended to help NASA program and project managers incorporate Small Business Innovat...
A broad overview of the scope of research presently being supported by NASA in aircraft propulsion i...
NASA has had a long history in fundamental and applied high lift research. Current programs provide ...
Through a robust partnership with the aviation industry, over the past 50 years NASA programs have h...
This report is intended to help NASA program and project managers incorporate Small Business Innovat...
The research and technology program of the civil air transportation system is reported. Research is ...
The Commercial Aero-Propulsion Control Working Group (CAPCWG), consisting of propulsion control tech...
Specific to the application of any technology to a vehicle, such as circulation control, it is impor...
Propulsion requirements were determined for 0.5 and 0.7 Mach aircraft. Sensitivity studies were cond...
In the past few years, NASA (National Aeronautics and Space Administration) Aeronautics Research Mis...
This is a quick presentation on the UAM Research Visions which include the Commerical Operating Envi...
The Aeronautics Test Program (ATP) within the National Aeronautics and Space Administration (NASA) A...
This presentation educates public and stakeholders on NASA organization, ARMD programs and projects,...
The Overarching Mission of NASA's Aeronautics Research Mission Directorate (ARMD) is: To advance U.S...
The NASA Aeronautics Research Mission Directorate (ARMD) is bringing together public, private, and a...
This report is intended to help NASA program and project managers incorporate Small Business Innovat...
A broad overview of the scope of research presently being supported by NASA in aircraft propulsion i...
NASA has had a long history in fundamental and applied high lift research. Current programs provide ...
Through a robust partnership with the aviation industry, over the past 50 years NASA programs have h...
This report is intended to help NASA program and project managers incorporate Small Business Innovat...
The research and technology program of the civil air transportation system is reported. Research is ...
The Commercial Aero-Propulsion Control Working Group (CAPCWG), consisting of propulsion control tech...
Specific to the application of any technology to a vehicle, such as circulation control, it is impor...
Propulsion requirements were determined for 0.5 and 0.7 Mach aircraft. Sensitivity studies were cond...