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The particular take-off distance required may be shorter than the available runway length. In this case a lower thrust may be used. Lower thrust settings increase engine life and reduce maintenance costs. The take-off thrust available from a civil engine is a constant value up to a particular ambient temperature.
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
Its fuel capacity was increased to 30,030 L (7,930 US gal) and its maximum takeoff weight to 93,000 kg (205,000 lb). It first flew in December 1996 and entered service with Monarch Airlines in April 1997. The A321's closest Boeing competitors are the 737-900/900ER, [94] and the 757-200. [27] In 2018, the A321 list price was US$118.3 million. [85]
The A321 entered service in January 1994 with Lufthansa; seen here is an A321-100. The Airbus A321 was the first derivative of the A320, also known as the Stretched A320, A320-500 and A325. [6] [7] Its launch came on 24 November 1988, around the same time as the A320 entered service, after commitments for 183 aircraft from 10 customers were ...
The maximum takeoff weight (MTOW) or maximum gross takeoff weight (MGTOW) or maximum takeoff mass (MTOM) of an aircraft, also known as the maximum structural takeoff weight or maximum structural takeoff mass, [1] is the maximum weight at which the pilot is allowed to attempt to take off, due to structural or other limits.
[citation needed] To offer similar takeoff performance, pitch response to stick input is a rate-command to hit the 3°/sec rotation rate to capture the right pitch attitude and there is an "electronic tail bumper" preventing a tailstrike if the stick is less than three-quarters of the way aft; additional thrust, slower rotation and lift-off ...
Remember the takeoff weight components contributions: O E W + P L + F O B = T O W {\displaystyle OEW+PL+FOB=TOW} Where OEW is the Operating Empty Weight (that is a charactersitic of the plane), PL is the Payload actually embarqued, and FOB the Fuel actually embarqued and TOW the actual take-off weight.
The payload fraction of modern twin-aisle aircraft is 18.4% to 20.8% of their maximum take-off weight, while single-aisle airliners are between 24.9% and 27.7%. An aircraft weight can be reduced with light-weight materials such as titanium , carbon fiber and other composite plastics if the expense can be recouped over the aircraft's lifetime.