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The Beriev Be-2500 Neptun (Russian: Бериев Бе-2500 «Нептун») is a super heavy amphibious transport aircraft that, as of 2007, was [needs update] in design and development by Russian design firm Beriev. The maximum takeoff weight is estimated at 2500 tons, hence its name.
Powered aircraft range is limited by the aviation fuel energy storage capacity (chemical or electrical) considering both weight and volume limits. [1] Unpowered aircraft range depends on factors such as cross-country speed and environmental conditions. The range can be seen as the cross-country ground speed multiplied by the maximum time in the ...
Type MTOW [kg] MLW [tonnes] TOR [m] LR [m] ICAO category FAA category; Antonov An-225: 640,000: 591.7: 3,500: Super: Super Scaled Composites Model 351 Stratolaunch
Beriev Be-2500: 1980s: 2460.57 tons Super heavy amphibious transport aircraft Beriev Be-5000 1980s: 4921.03 tons Twin fuselage Be-2500 McDonnell Douglas MD-12: 1990: 423.21 tons Proposed double deck airliner, canceled in mid-1990s Boeing New Large Airplane: 1990s: 523.6 tons 747 replacement powered by 777 engines, canceled in the 1990s Aerocon ...
Single engine piston aircraft with tricycle landing gear [1]; Model Engine Power hp Seats Wing Sq. Ft. MTOW lb Empty lb Cruise knots Range nmi AS 202 Bravo NG: L. AEIO-360: 180: 3: 149: 2,202: 1,389
The report states that a B-21 could fly 2,500 miles (4,000 km) without refueling while carrying more munitions as compared to the maximum 930 miles (1,500 km) range of the RAAF's F-35 fighter jets, which require air-to-air refueling. A single B-21 can also deliver the same impact as several F-35As.
The following is the list of purpose-built passenger jet airliners.It excludes turboprop and reciprocating engine powered airliners. It also excludes business jets and aircraft designed primarily for the transportation of air cargo.
Lockheed YF-94 (S/N 48-373). This was the second aircraft built (from TF-80C) On 16 April 1949, the first YF-94 prototype performed its maiden flight. [6] To accelerate development, these early test aircraft were converted from existing T-33s; they maintained roughly 75% commonality in terms of components with those used in the earlier F-80 and T-33As.