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  1. The de Havilland Goblin, originally designated as the Halford H-1, is an early turbojet engine designed by Frank Halford and built by de Havilland. The Goblin was the second British jet engine to fly, after Whittle's Power Jets W.1 , and the first to pass a type test and receive a type certificate issued for an aircraft propulsion ...

  2. El Goblin fue el motor primario del de Havilland Vampire, y debió haber sido el motor del P-80 Shooting Star (como el Allis-Chalmers J36) antes de que los diseñadores cambiasen de motores debido a retrasos en la producción. El Goblin también motorizó al Saab 21R, al Fiat G.80 y al de Havilland Swallow.

  3. Hace 3 días · The Army used an H-1 engine as the power plant in the prototype XP-80, but replaced it with the more powerful, 17,792 N (4,000 lb.) thrust GE I-40 (J33). Subsequently the Navy contracted with Allis-Chalmers for construction of 40 H-1 engines, known as the J36.

  4. 10 de sept. de 2020 · Goblin engine. For de Havilland to set up its own aero engine company was an indication of how rapidly it had progressed in this field. From making engines for its own light aeroplanes, DH was soon producing a pioneering jet — and the same man, Frank Halford, was behind them all.

  5. GENERAL CHARACTERISTICS: Engine Type: Centrifugal 16 compressor turbojet. First engine delivered: November 1948. Number built: 2,688. Performance: Maximum Thrust: 3,500 lb. (15.6 kN) at 10,200 rpm. Turbine: Single-stage axial flow. Length: 107 inches (271.8 cm) Diameter: 50 inches (127 cm) Dry weight: 1,550 lbs. (703 kg)

  6. El de Havilland Goblin, originalmente Halford H-1, es uno de los primeros turborreactores, diseñado por Frank Halford. El Goblin construido por de Havilland fue el segundo reactor británico en volar, y el primero en pasar las pruebas y recibir la clasificación de "turbina de gas".

  7. The de Havilland Goblin 35 centrifugal flow jet engine was used to power the two seat DH115 Vampire Trainer used for advanced training in Britain and overseas. Engine specifications: Static Thrust: 3,500 lb. Air Mass Flow Rate: 62.5 lbs/sec. Pressure Ratio: 3.62:1. First engine delivered: November 1948. Number built: 2,688.