Consideration is given to the design phase of the highly maneuverable aircraft technology program. Design objectives are examined, noting full-scale design and the remotely piloted research vehicle. Attention is given to subsonic, transonic, and supersonic design. Design results are discussed with reference to aerodynamic efficiency, aeroelastic tailoring, and the flight test program.
HiMAT aerodynamic design and flight test experience
Flight Testing Conference ; 1981 ; Las Vegas, NV
1981-11-01
Conference paper
No indication
English
HiMAT aerodynamic design and flight test experience
AIAA | 1981
|Qualification of HiMAT flight systems
NTRS | 1980
|