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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.
It continued in primarily NASA test operations until September 2003. The shortest takeoff distance was achieved with the nacelles at 75 degrees angle. [8] After N703NA was retired from test operations, it was donated to the Smithsonian National Air and Space Museum in Washington, D.C. The XV-15 was flown cross-country from Fort Worth, Texas to ...
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: ...
In 2017 the aircraft set a new STOL world record at Valdez, with a take off in 13 feet 8 inches, and a landing in 10 feet 5 inches. [3] In 2018, the aircraft set a new STOL world record at Valdez, with a take off in 11 ft 0 inches. [4]
Aircraft records. 1 language ... This article gives yearly aviation records under 5 headings: airspeed, range, ceiling, gross take-off weight, and engine power. Year ...
[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]
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 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]