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The F-2 has three display screens, including a liquid crystal display from Yokogawa. Differences between F-2 and F-16 block 40. Mitsubishi used the existing F-16 design as a reference guide for design work, and more than 95% of F-16 engineering drawings are changed for F-2. [24] [25] Some differences in the F-2 from the F-16A: a 25% larger wing ...
The modified F-16 demonstrated a maximum speed of Mach 2.0 (Mach 2.0 is the F-16's clean certified maximum speed) and handling characteristics similar to a normal F-16. Subsonic specific excess power was slightly improved. The trade studies involved additional CFD, testing, and weight and cost analyses.
The F-16E (single seat) and F-16F (two seat) are newer F-16 Block 60 variants based on the F-16C/D Block 50/52. The United Arab Emirates invested heavily in their development. They feature improved AN/APG-80 active electronically scanned array (AESA) radar, infrared search and track (IRST), avionics, conformal fuel tanks (CFTs), and the more ...
[31] [35] The glove covered over 5 square feet (0.46 m 2) of the wing. Overall, F-16XL-1 completed 31 test flights for these tests from May 1990 to September 1992. [32] Afterwards, it was used to test takeoff performance, engine noise, and sonic boom phenomena. [36] F-16XL-2 had its engine replaced with the more powerful General Electric F110-129.
Whereas the premier third-generation jet fighters (e.g., the F-4 and MiG-23) were designed as interceptors with only a secondary emphasis on maneuverability, 4th generation aircraft try to reach an equilibrium, with most designs, such as the F-14 and the F-15, being able to execute BVR interceptions while remaining highly maneuverable in case the platform and the pilot find themselves in a ...
Pages in category "General Dynamics F-16 Fighting Falcon" The following 18 pages are in this category, out of 18 total. ... Mitsubishi F-2; 2015 Moncks Corner mid-air ...
The concept, slim and high-power, resulted in an approximately 30% higher thrust per unit cross-sectional area compared to the GE F110 the Mitsubishi F-2 is equipped with. To achieve this thrust level, a higher combustion temperature (1,800°C class) and an optimized aerodynamic design were needed, which in turn required advanced material ...
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