Английская Википедия:Bradley BA-200 ATAC

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The Bradley BA-200 ATAC (or Bradley ATAC BA-200) was an American homebuilt aircraft that was designed by Bradley Aerospace of Chico, California, introduced in the mid-1990s. The aircraft was intended to be supplied as a kit for amateur construction, but is likely that only one was constructed.[1]

Design and development

The BA-200 was conceived as a follow-on design to the Bradley Aerobat. It was intended to feature two-seats-in-tandem and aerobatic capabilities that included an airframe stressed to +/-15g.[1]

The aircraft was made from all-metal construction. Its Шаблон:Convert span wing had a wing area of Шаблон:Convert. The cabin width was Шаблон:Convert. The acceptable power range was Шаблон:Convert and the standard engine used was the Шаблон:Convert Volkswagen air-cooled engine .[1]

The aircraft had a typical empty weight of Шаблон:Convert and a gross weight of Шаблон:Convert, giving a useful load of Шаблон:Convert. With full fuel of Шаблон:Convert the payload for the pilot, passenger and baggage was Шаблон:Convert.[1]

The standard day, sea level, no wind, take off with a Шаблон:Convert engine was Шаблон:Convert and the landing roll was Шаблон:Convert.[1]

The manufacturer estimated the construction time from the supplied kit as 200 hours.[1]

Operational history

By 1998 the company reported that one aircraft had been completed and was flying.[1]

In April 2015 no examples were registered in the United States with the Federal Aviation Administration and it is unlikely that any exist any more.[2]

Specifications (BA-200)

Шаблон:Aircraft specs

See also

References

Шаблон:Reflist

Шаблон:Bradley Aerospace aircraft Шаблон:Aerobatics

  1. 1,0 1,1 1,2 1,3 1,4 1,5 1,6 Purdy, Don: AeroCrafter - Homebuilt Aircraft Sourcebook, Fifth Edition, page 347. BAI Communications, 15 July 1998. Шаблон:ISBN
  2. Шаблон:Cite web