Harrier Jump Jet Compressor Casing Table - Rolls Royce Pegasus Engine - OVAL | AEROART.CO.UK

 

Now only a few left, for sale is this amazing coffee table crafted from a High Pressure Compressor Casing from a Rolls-Royce Pegasus engine as used in the Harrier Jump Jet. 

     The Harrier Jump Jet is an attack aircraft capable of vertical and short takeoff and landing operations.  Named after a bird of prey, designed and manufactured by Hawker Siddeley and powered by the Rolls-Royce Pegasus engine the Harrier soon became a legend of the 20th century.  Most notable was its formidable success rate in the Falkland Islands during the Argentinian war where Sea Harriers shot down 20 mirage jets while losing 0 aircraft in air-to-air combat. 

     

       Topped in 10mm toughened glass

       Rare & Historical 

 

Specifications : Harrier GR.3

 

General characteristics

  • Crew: 1
  • Length: 46 ft 10 in (14.27 m)
  • Wingspan: 25 ft 5 in (7.75 m) 
29 ft 8 in (9 m) with ferry tips fitted
  • Height: 11 ft 11 in (3.63 m)
  • Wing area: 201.1 sq ft (18.68 m2) 
216 sq ft (20 m2) with ferry tips fitted
  • Aspect ratio: 3.175
4.08 with ferry tips fitted
  • Airfoil: root: Hawker 10% ; tip: Hawker 3.3%[189]
  • Empty weight: 13,535 lb (6,139 kg)
  • Max takeoff weight: 55,556 lb (25,200 kg)
  • Fuel capacity: 5,060 lb (2,295 kg) internal
2x 100 imp gal (120 US gal; 450 l) (790 lb (358 kg)) drop-tanks for combat
2x 330 imp gal (400 US gal; 1,500 l) (2,608 lb (1,183 kg)) drop-tanks for ferry

Performance

  • Maximum speed: 635 kn (731 mph; 1,176 km/h) at sea level
  • Maximum diving speed: Mach 1.3
  • Combat range: 360 nmi (414 mi; 667 km) ho-lo-hi with 4,400 lb (1,996 kg) payload
200 nm (1.2×10−10 mi; 2.0×10−10 km) lo-lo with 4,400 lb (1,996 kg) payload
  • Ferry range: 1,850 nmi (2,129 mi; 3,426 km) with 330 imp gal (400 US gal; 1,500 l) drop-tanks
3,000 nmi (3,500 mi; 5,600 km) with one AAR
  • Endurance: 1 hour 30 minutes combat air patrol 100 nmi (120 mi; 190 km) from base.
7 hours plus with one AAR
  • Service ceiling: 51,200 ft (15,600 m)
  • g limits: +7.8 -4.2
  • Time to altitude: 40,000 ft (12,192 m) in 2 minutes 23 seconds from a vertical take-off
  • Take-off run CTOL: 1,000 ft (300 m) at max TO weight

Armament




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