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De Havilland Swallow




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The De Havilland DH.108 "Swallow" was an Experimental Aircraft designed in October 1945 . A Flying Wing , it was designed to evaluate Swept-wing handling characteristics at subsonic speeds.


DEVELOPMENT

The first DH.108 Prototype , ''TG283'', utilizing the De Havilland Vampire fuselage and a 43° swept wing flew on May 15, 1946 . It was capable of only 280 mph (451 km/h) and was lost in a crash on May 1 , 1950 . The second prototype, ''TG306'', with a 45° swept wing with automatic leading-edge slats and a De Havilland Goblin 3 Turbojet flew in June 1946 . It was expected to break the air speed record of the day, 616 mph (991 km/h). Unfortunately, on September 27, 1946, the Airframe suffered a catastrophic Structural Failure at Mach 0.9. Pilot Geoffrey De Havilland Jr , son of de Havilland owner-designer Geoffrey De Havilland was killed in the accident. ''VW120'', the third and final prototype with a more pointed nose and aerodynamic canopy first flew on July 24, 1947 . On April 12, 1948 this aircraft established a new world speed record on a 100 km (62 mi) circuit of 974.02 km/h (604.98 mph). Then, on September 9, 1948 it exceeded the speed of sound in a shallow dive from 12,195 m (40,000) ft to 9,145 m (30,000) ft. The first British aircraft to exceed Mach 1, the DH.108 was also the first jet-powered aircraft in the world to do so, as the earlier Bell X-1 and Douglas Skyrocket were Rocket -powered. The third prototype was also lost in a crash.


SPECIFICATIONS (DH.108 3RD PROTOTYPE)



General characteristics

  • Crew: One

  • Length: 8.17 m (26 ft 10 in)

  • Wingspan: 11.89 m (39 ft 0 in)

  • Height: 4.27 m (14 ft 0 in)

  • Wing area: 30.47 m² (327.86 ft²)

  • Loaded weight: 4,064 kg (8,940 lb)

  • Powerplant: 1x De Havilland Goblin 4, 16.67 kN (3,738 lbf) thrust

  • Performance

  • Maximum speed: 1,090 km/h (677 mph)

  • Service ceiling: 10,800 m (35,425 ft)

  • Wing Loading : 133 kg/m² (27 lb/ft²)

  • Thrust/weight : 0.42



REFERENCES



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