To install click the Add extension button. That's it.

The source code for the WIKI 2 extension is being checked by specialists of the Mozilla Foundation, Google, and Apple. You could also do it yourself at any point in time.

4,5
Kelly Slayton
Congratulations on this excellent venture… what a great idea!
Alexander Grigorievskiy
I use WIKI 2 every day and almost forgot how the original Wikipedia looks like.
Live Statistics
English Articles
Improved in 24 Hours
Added in 24 Hours
What we do. Every page goes through several hundred of perfecting techniques; in live mode. Quite the same Wikipedia. Just better.
.
Leo
Newton
Brights
Milds

From Wikipedia, the free encyclopedia

D-292
The U.S. Army Bell D-292 conducting a flight test
Role Experimental helicopter
National origin United States
Manufacturer Bell Helicopter
First flight 30 August 1985
Number built 1
Developed from Bell 222

The Bell D-292 was an American experimental helicopter developed by Bell Helicopters for the United States Army Advanced Composite Airframe Program (ACAP), as part of the studies involved in the Light Helicopter Experimental (LHX) program.

YouTube Encyclopedic

  • 1/3
    Views:
    77 110
    1 806
    5 636
  • Helicopter Fatal Accident - THE PILOT'S POOR IN-FLIGHT DECISION TO LAND DOWNWIND
  • #292 "any particular helicopter that’s in a higher demand for pilots?"
  • #273 - Helicopter Landing (set downs) For Those That Struggle

Transcription

Design and development

The Bell D-292 was developed under the US Army's Advanced Composite Airframe Program (ACAP), which was a project to develop an all-composite helicopter fuselage, considerably lighter and less costly to build than predominantly metal airframes, in support of the LHX program.[1][2] In February 1981, contracts were awarded to Sikorsky and Bell Helicopters, with Sikorsky submitting the S-75.[3] Both companies were to build three airframes, one tool-proof version, one static-test version and a flight-test vehicle.[3]

The Bell D-292 used the Avco Lycoming engines, transmission, two-bladed main and tail rotors, tailboom, vertical fin, and rotor pylon from the Bell 222. The new airframe replaced metal with composites for greater strength, reduced weight and both lower manufacturing and maintenance costs.

The D-292 serial number 85-24371 flew for the first time on 30 August 1985[4] following delays due to funding and industrial problems.[3]

Specifications

General characteristics

  • Crew: four
  • Length: 40 ft 5 in (12.32 m)
  • Height: 11 ft 2 in (3.40 m)
  • Empty weight: 5,765 lb (2,615 kg)
  • Max takeoff weight: 7,485 lb (3,395 kg)
  • Powerplant: 2 × Avco Lycoming LTS 101-750C-1 turboshaft, 684 hp (510 kW) each
  • Main rotor diameter: 42 ft 0 in (12.80 m)

See also

Related development

Aircraft of comparable role, configuration, and era

Related lists

References

Notes

  1. ^ Harding 1997
  2. ^ Historic US Army Helicopters Archived 2007-02-24 at the Wayback Machine
  3. ^ a b c "Bell admits ACAP delays". Flight International. 1985-01-12.
  4. ^ "Bell ACAP takes off". Flight International: 9. 1985-09-21.

Bibliography

This page was last edited on 11 April 2023, at 17:49
Basis of this page is in Wikipedia. Text is available under the CC BY-SA 3.0 Unported License. Non-text media are available under their specified licenses. Wikipedia® is a registered trademark of the Wikimedia Foundation, Inc. WIKI 2 is an independent company and has no affiliation with Wikimedia Foundation.