Samiksha Jaiswal (Editor)

Atlas ACE

Updated on
Edit
Like
Comment
Share on FacebookTweet on TwitterShare on LinkedInShare on Reddit
Top speed
  
555 km/h

Length
  
11 m

Wingspan
  
11 m

First flight
  
April 29, 1991

Atlas ACE httpsmybroadbandcozavbattachmentphpattach

Manufacturer
  
Atlas Aircraft Corporation

The Atlas ACE is a South African turboprop trainer, that was designed by the Atlas Aircraft Corporation as a contender to replace the North American Harvard in service with the South African Air Force. The aircraft was not selected and only two examples were completed.

Contents

Design and development

The design originated as the 1986 Project Ovid by the government research agency Aerotek, as a composites technology demonstrator. In 1991 the design was entered into a competition to replace the North American Harvard by the Atlas Aircraft Corporation as the ACE (All Composite Evaluator).

The ACE is a tandem two-seat low-wing cantilever monoplane powered by a Pratt & Whitney PT6A turboprop. It has a retractable nosewheel landing gear and a conventional tail unit. The aircraft is constructed from carbon fiber composites.

The prototype was first flown on 29 April 1991, but did not win the competition which was awarded to the Pilatus PC-7.

On 14 January 1995 the prototype was lost in a wheels up landing at Jan Smuts Airport. The second improved aircraft was scheduled to fly, but the design was not developed.

Specifications

General characteristics

  • Crew: 2
  • Length: 35 ft 5 in (10.8 m)
  • Wingspan: 35 ft 5 in (10.8 m)
  • Wing area: 193.75 ft2 (18 m2)
  • Empty weight: 3406 lb (1545 kg)
  • Gross weight: 4850 lb (2200 kg)
  • Powerplant: 1 × Pratt & Whitney PT6A-34, 750 hp (559 kW)
  • Performance

  • Maximum speed: 345 mph (555 km/h)
  • Range: 1266 miles (2037 km)
  • Service ceiling: 33,000 ft (10,000 m)
  • Rate of climb: 2750 ft/min (838 m/s)
  • References

    Atlas ACE Wikipedia