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The flight time of 15h 8m giving an average speed of almost exactly 200 km/h. [61] [62] March 21, 1999: 40,814 km: Bertrand Piccard and Brian Jones: Breitling Orbiter: Distance record for a balloon: January 31, 2015: 10,711 km: Troy Bradley and Leonid Tiukhtyaev: Two Eagles Balloon: Distance record for a straight gas balloon: April 23, 1988: ...
Bridgeman, Leonard Jane's All The World's Aircraft 1948. MacMillan, 1948. Bridgeman, Leonard Jane's All The World's Aircraft 1959–60. Sampson, Low, Marston and Company, 1959. Fillingham, Paul Basic Guide to Flying. New York: Hawthorn, 1975. ISBN 0-801-50525-9; Jackson, Paul Janes All the Worlds Aircraft 2004–05, Janes Publishing Company, 2004.
[31] [32] [33] in a scheduled time of 16 hours and 20 minutes. [34] [35] As of 2023, it continues to hold the record for the longest ever scheduled commercial nonstop flight (by great circle distance) as well as the world's longest domestic flight. [36] [37] [38] [39]
The speed will ensure the aircraft achieves the required height above the takeoff surface within the takeoff distance. [citation needed] To achieve a balanced field takeoff, V 1 is selected so the take-off distance with one engine inoperative, and the accelerate-stop distance, are equal. [1]
STOL (Short Take Off and Landing). STOL performance of an aircraft is the ability of aircraft to take off and clear a 50-foot obstruction in a distance of 1,500 feet from beginning the takeoff run. It must also be able to stop within 1,500 feet after crossing a 50-foot obstacle on landing. —
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.
Takeoff weight is the weight of an aircraft as it takes off partway along a runway. Few flight planning systems calculate the actual takeoff weight; instead, the fuel used for taking off is counted as part of the fuel used for climbing up to the normal cruise height. Landing weight is the weight of an aircraft as it lands at the destination ...
Conversely, a lower V 1 leads to a longer takeoff distance with one-engine-inoperative, and a shorter accelerate-stop distance. It seems what he meant to write was this: A higher V 1 leads to a shorter remaining takeoff distance with when one engine becomes inoperative at that speed, and a higherlonger required accelerate-stop distance at that ...