The Global Sentry is a high altitude reconnaissance aircraft design for the NASA/USRA design project. The Global Sentry uses proven technologies, light-weight composites, and meets the R.F.P. requirements. The mission requirements for the Global Sentry are described. The configuration option is discussed and a description of the final design is given. Preliminary sizing analyses and the mass properties of the design are presented. The aerodynamic features of the Global Sentry are described along with the stability and control characteristics designed into the flight control system. The performance characteristics are discussed as is the propulsion installation and system layout. The Global Sentry structural design is examined, including a wing structural analysis. The cockpit, controls and display layouts are covered. Manufacturing is covered and the life cost estimation. Reliability is discussed. Conclusions about the current Global Sentry design are presented, along with suggested areas for future engineering work.
Global Sentry: NASA/USRA high altitude reconnaissance aircraft design, volume 2
1990-01-01
Report
No indication
English
NASA/USRA High Altitude Reconnaissance Aircraft
NTIS | 1990
|NASA/USRA high altitude reconnaissance aircraft
NTRS | 1990
|NASA/Usra Advanced Design Program
NTIS | 1992
NASA/USRA advanced design program
NTRS | 1992