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test flight - перевод на голландский
![Flight test engineer's workstation aboard an [[Airbus A380]] prototype](https://commons.wikimedia.org/wiki/Special:FilePath/A380 teststation fb06rs.jpg?width=200 "Flight test engineer's workstation aboard an [[Airbus A380]] prototype")
![Static pressure probe rig aboard [[Boeing 747-8I]] prototype; a long plastic tube, shown wound round a storage drum, is connected to a probe with static pressure orifices. The probe is trailed about two wing spans behind the aircraft.<ref>AGARD-AG-160-VOL-2, AGARD flight test instrumentation series. Volume 2: In-flight temperature measurements, p.30</ref>](https://commons.wikimedia.org/wiki/Special:FilePath/Boeing 747-8I prototype static pressure probe.jpg?width=200 "Static pressure probe rig aboard [[Boeing 747-8I]] prototype; a long plastic tube, shown wound round a storage drum, is connected to a probe with static pressure orifices. The probe is trailed about two wing spans behind the aircraft.<ref>AGARD-AG-160-VOL-2, AGARD flight test instrumentation series. Volume 2: In-flight temperature measurements, p.30</ref>")
![Pressure measurement equipment and water tanks in [[Boeing 747-8I]] prototype](https://commons.wikimedia.org/wiki/Special:FilePath/Cabin nose section of 747-8I prototype.jpg?width=200 "Pressure measurement equipment and water tanks in [[Boeing 747-8I]] prototype")
![Static pressure probe on the nose of a [[Sukhoi Superjet 100]] prototype](https://commons.wikimedia.org/wiki/Special:FilePath/Sukhoi Superjet 100 prototype.jpg?width=200 "Static pressure probe on the nose of a [[Sukhoi Superjet 100]] prototype")
![[[Concorde]] on March 2, 1969](https://commons.wikimedia.org/wiki/Special:FilePath/02.03.69 1er vol de Concorde (1969) - 53Fi1931 - cropped.jpg?width=200 "[[Concorde]] on March 2, 1969")
![[[Airbus A380]] on April 27, 2005](https://commons.wikimedia.org/wiki/Special:FilePath/1er vol de l' A380.jpg?width=200 "[[Airbus A380]] on April 27, 2005")
![''[[Wright Flyer]]'' on December 17, 1903](https://commons.wikimedia.org/wiki/Special:FilePath/Wright First Flight 1903Dec17 (full restore 115).jpg?width=200 "''[[Wright Flyer]]'' on December 17, 1903")
Определение
Википедия
Flight testing is a branch of aeronautical engineering that develops specialist equipment required for testing aircraft behaviour and systems. Instrumentation systems are developed using proprietary transducers and data acquisition systems. Data is sampled during the flight of an aircraft, or atmospheric testing of launch vehicles and reusable spacecraft. This data is validated for accuracy and analyzed before being passed to specialist engineering groups for further analysis to validate the design of the vehicle.
The flight test phase accomplishes two major tasks: 1) finding and fixing any design problems and then 2) verifying and documenting the vehicle capabilities for government certification or customer acceptance. The flight test phase can range from the test of a single new system for an existing vehicle to the complete development and certification of a new aircraft, launch vehicle, or reusable spacecraft. Therefore, the duration of a particular flight test program can vary from a few weeks to many years.
