X-47 Pegasus

From Wikipedia, the free encyclopedia

X-47A rollout
Enlarge
X-47A rollout
X-47B over sea (CG concept)
Enlarge
X-47B over sea (CG concept)
Northrop Grumman X-47B
Enlarge
Northrop Grumman X-47B

The Northrop Grumman X-47A Pegasus is a demonstration Unmanned Combat Aerial Vehicle. The X-47 is part of DARPA's J-UCAS project.

Unlike the Boeing X-45, Pegasus development was company-funded. The initial vehicle carries the designation X-47A; a follow-on Naval version is designated X-47B.

The proof-of-concept X-47A vehicle was built under contract by Burt Rutan's Scaled Composites at the Mojave Spaceport. The roll out ceremony at Mojave was in July 2001 and the first flight was successfully completed in February 2003. The program was terminated on January 13, 2006 as part of the US Military's Quadrennial Defense Review.

[edit] Specifications (X-47A)

General characteristics

  • Crew: none
  • Length: 19 ft 7 in (8.50 m)
  • Wingspan: 19 ft 6 in (8.47 m)
  • Height: 6 ft 1 in (1.86 m)
  • Wing area: ft² (m²)
  • Empty weight: 3,836 lb (1,740 kg)
  • Loaded weight: 4,877 lb (2,212 kg)
  • Max takeoff weight: 5,903 lb (2,678 kg)
  • Powerplant:Pratt & Whitney JT15D-5C (X-45A)
    Pratt & Whitney F100-220 (X-45B) turbofan, 3,190 lbf (14.2 kN)

Performance

Armament

None

[edit] External links

[edit] Related content

 

 

Designation sequence

X-44 - X-45 - X-46 - X-47 - X-48 - X-49 - X-50

 

See also



In other languages