Miles Sparrowjet

From Wikipedia, the free encyclopedia

M.77 Sparrowjet
Type racing
Manufacturer Miles Aircraft
Number built 1
Developed from Miles Sparrowhawk


The Miles M.77 Sparrowjet was a twin-engined jet-powered racing aeroplane built by Miles Aircraft by fitting Turbomeca Palas jets to the prototype Miles Sparrowhawk. The conversion commenced in December 1950 and the Sparrowjet first flew on 14 December, 1953. Other modifications included a new tail section and front fuselage (in place of the Sparrowhawk's single engine), fixed, faired-in undercarriage and a large clear canopy. The wing roots were modified to take the Palas engines.

The Sparrowjet won the SBAC Challenge Cup at Yeadon, West Yorkshire in 1956 and the King's Cup in 1957 with a top speed of 228 mph (367 km/h). In 1964 the Sparrowjet was destroyed in a hangar fire.

Contents

[edit] Specifications (Sparrowjet)

[edit] General characteristics

  • Crew: one pilot
  • Length: 30 ft 10 in (9.40 m)
  • Wingspan: 28 ft 6 in (8.69 m)
  • Height: ft in ( m)
  • Wing area: 156 ft² (14.5 m²)
  • Empty: 1,578 lb (717 kg)
  • Loaded: 2,400 lb (1,090 kg)
  • Maximum takeoff: lb ( kg)
  • Powerplant: 2x Turbomeca Palas, 330 lbf (1.5 kN) thrust each

[edit] Performance

  • Maximum speed: 230 mph (368 km/h)
  • Range: 270 miles (432 km)
  • Service ceiling: ft ( m)
  • Rate of climb: 2,100 ft/min (640 m/min)
  • Wing loading: 15 lb/ft² (75 kg/m²)
  • Thrust-to-weight: 1.4 N/kg

[edit] Related content

Related development: Miles Sparrowhawk

Comparable aircraft:

Designation sequence: M.69 "Marathon" - M.7 "Merchantman"1 - M.75 "Ariews" - M.77 "Sparrowjet" - M.100 "Student"