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Smart Skies Project The Smart Skies Project is a leading edge research program exploring the research and development of future technologies that support the efficient utilisation of airspace by both manned and unmanned aircraft. It focused upon the exploration and development of three key enabling aviation technologies – an automated ...
Earlier, data from a Trident's quick access recorder had provided the Air Accidents Investigation Branch (AAIB) with useful supplemental data over-and-above that of the aircraft's flight data recorder that helped the diagnosing of the cause of the 1972 British European Airways Flight 548, the "Staines air disaster" where the Trident's leading ...
The CFM International LEAP ("Leading Edge Aviation Propulsion") is a high-bypass turbofan engine produced by CFM International, a 50–50 joint venture between American GE Aerospace and French Safran Aircraft Engines. It is the successor of the CFM56 and competes with the Pratt & Whitney PW1000G to power narrow-body aircraft.
NASA's first X-plane in over a decade, it is part of NASA's New Aviation Horizons initiative, which will also produce up to five larger-scale aircraft. The X-57 was built by the agency's SCEPTOR project, over a four-year development period at Armstrong Flight Research Center, California, with a first flight initially planned for 2017. [14] [15 ...
The Open Group Future Airborne Capability Environment (FACE Consortium) was formed in 2010 to define an open avionics environment for all military airborne platform types. . Today, it is a real-time software-focused professional group made up of industry suppliers, customers, academia, and us
The triple-slotted trailing edge flaps are well displayed and the Krueger flaps on the leading edge also are visible. In aircraft design and aerospace engineering, a high-lift device is a component or mechanism on an aircraft's wing that increases the amount of lift produced by the wing. The device may be a fixed component, or a movable ...
The leading edge is the part of the wing that first contacts the air; [1] [2] alternatively it is the foremost edge of an airfoil section. [3] The first is an aerodynamic definition, the second a structural one.
Aviation Week postulates that these elements suggest the designers have avoided "highly sensitive technologies" due to the near certainty of eventual operational loss inherent with a single engine design and a desire to avoid the risk of compromising leading edge technology. [14]