Lockheed Tri Star (RAF) - Specifications (TriStar K1)

Specifications (TriStar K1)

Data from The International Directory of Military Aircraft, RAF TriStar page Airliners.net

General characteristics

  • Crew: 4 (1 captain, 1 co-pilot, 1 air engineer, 1 Air Loadmaster)
  • Capacity: 187 passengers (250 on C variant)
  • Length: 50.05 m (164 ft 3 in)
  • Wingspan: 50.09 m (164 ft 4 in)
  • Height: 16.87 m (55 ft 4 in)
  • Wing area: 329.0 m² (3540 ft²)
  • Empty weight: 105,165 kg (242,684 lb)
  • Max. takeoff weight: 245,000 kg (540,000 lb)
  • Powerplant: 3 × Rolls-Royce RB.211-524B turbofans, 50,000 lbf (222.4 kN) each
  • Maximum Fuel Load: 136,080 kg (300,000 lb)

Performance

  • Maximum speed: Mach 0.90
  • Cruise speed: Mach 0.83 (483 kn, 894 km/h)
  • Range: 4,200 nmi (7,785 km) with maximum passenger payload
  • Service ceiling: 43,000 ft (13,000 m)
  • Rate of climb: 2,820 ft/min (14.3 m/s)

Read more about this topic:  Lockheed Tri Star (RAF)