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Adam A700 AdamJet

From Biocrawler, the free encyclopedia.

The Adam A700 AdamJet is a six-seat civil utility aircraft currently under development. The aircraft has been developed in parallel with the generally similar Adam A500, although while that aircraft is piston-engined, the A700 is powered by two Williams FJ33 turbofans.

The prototype first flew on July 28 2003.

Contents

Specifications (A500)

General characteristics

  • Crew: one, pilot
  • Capacity: five passengers
  • Length: 40 ft 9 in (12.42 m)
  • Wingspan: 44 (13.41 m)
  • Height: 9 ft 7 in (2.93 m)
  • Wing area: ft² ( m²)
  • Empty: lb ( kg)
  • Loaded: lb ( kg)
  • Maximum takeoff: lb ( kg)
  • Powerplant: 2x Williams FJ33, 1,100 lbf (4.9 kN) each

Performance

  • Maximum speed: 382 mph (612 km/h)
  • Range: 1,654 miles (2,646 km)
  • Service ceiling: 41,000 ft (12,500 m)
  • Rate of climb: ft/min ( m/min)
  • Wing loading: lb/ft² ( kg/m²)
  • Thrust/weight:

Related content

Related development: Adam M-309 - Adam A700


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Wikipedia (http://en.wikipedia.org/wiki/Main_Page) Adam_A700_AdamJet (http://en.wikipedia.org/wiki/Adam_A700_AdamJet) version history (http://en.wikipedia.org/w/index.php?title=Adam_A700_AdamJet&action=history) GNU Free Documentation Lizenz (http://en.wikipedia.org/wiki/Wikipedia:Text_of_the_GNU_Free_Documentation_License) CC-by-sa (http://creativecommons.org/licenses/by-sa/2.5/)

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