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- Westinghouse_J40 abstract "The Westinghouse J40 was to be a high performance afterburning turbojet engine. It was intended by the Bureau of Aeronautics, in early 1946, to power several fighter aircraft, with a rating of 7,500 lbf (33 kN) thrust at sea level static conditions, but a more powerful 11,000 lbf (49 kN) thrust version for the McDonnell F3H Demon proved to be a failure. After a troublesome and delayed development program, failures in service led to the loss of aircraft and pilots and grounding of all J40 powered aircraft.After the program was called a "fiasco" and an "engine flop", the J40 program was terminated in 1955, by which time all the aircraft it was to power were either grounded, cancelled or redesigned to use alternative engines. The J40's failure was among those that affected the most military programs and produced the most unflyable aircraft, and would lead to the downfall of the engine division of Westinghouse. In 1953 Westinghouse worked with Rolls-Royce to offer engines based on the Avon, but Westinghouse was out of the aircraft engine business when this engine also failed to find a United States market.".
- Westinghouse_J40 thumbnail XF3H_CVA-43.jpg?width=300.
- Westinghouse_J40 wikiPageExternalLink 1-292308-1490368.php.
- Westinghouse_J40 wikiPageExternalLink b-66.htm.
- Westinghouse_J40 wikiPageID "6593522".
- Westinghouse_J40 wikiPageRevisionID "604221255".
- Westinghouse_J40 combustion Combustor.
- Westinghouse_J40 compression "5.2".
- Westinghouse_J40 compressor "Single-Spool, 10 stage Axial".
- Westinghouse_J40 diameter "40.0".
- Westinghouse_J40 hasPhotoCollection Westinghouse_J40.
- Westinghouse_J40 length "300.0".
- Westinghouse_J40 lists "*List of aircraft engines".
- Westinghouse_J40 majorApplications McDonnell_F3H_Demon.
- Westinghouse_J40 manufacturer Westinghouse_Aviation_Gas_Turbine_Division.
- Westinghouse_J40 nationalOrigin United_States.
- Westinghouse_J40 programCost "2.81E8".
- Westinghouse_J40 specfuelcon "0.94".
- Westinghouse_J40 thrust "7500".
- Westinghouse_J40 weight "2.14".
- Westinghouse_J40 turbine "Two stage".
- Westinghouse_J40 type Turbojet.
- Westinghouse_J40 type "Afterburning Turbojet".
- Westinghouse_J40 weight "3500.0".
- Westinghouse_J40 subject Category:Abandoned_military_aircraft_engine_projects_of_the_United_States.
- Westinghouse_J40 subject Category:Engineering_failures.
- Westinghouse_J40 subject Category:Turbojet_engines_1940–1949.
- Westinghouse_J40 subject Category:Westinghouse_aircraft_engines.
- Westinghouse_J40 comment "The Westinghouse J40 was to be a high performance afterburning turbojet engine. It was intended by the Bureau of Aeronautics, in early 1946, to power several fighter aircraft, with a rating of 7,500 lbf (33 kN) thrust at sea level static conditions, but a more powerful 11,000 lbf (49 kN) thrust version for the McDonnell F3H Demon proved to be a failure.".
- Westinghouse_J40 label "Westinghouse J40".
- Westinghouse_J40 label "Westinghouse J40".
- Westinghouse_J40 label "Westinghouse J40".
- Westinghouse_J40 label "Westinghouse J40".
- Westinghouse_J40 sameAs Westinghouse_J40.
- Westinghouse_J40 sameAs Westinghouse_J40.
- Westinghouse_J40 sameAs Westinghouse_J40.
- Westinghouse_J40 sameAs m.0gd001.
- Westinghouse_J40 sameAs Q505865.
- Westinghouse_J40 sameAs Q505865.
- Westinghouse_J40 wasDerivedFrom Westinghouse_J40?oldid=604221255.
- Westinghouse_J40 depiction XF3H_CVA-43.jpg.
- Westinghouse_J40 isPrimaryTopicOf Westinghouse_J40.
