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- Flader_J55 abstract "The Flader J55, also known as the 124 within the company, was a small turbojet engine notable for its use of a supersonic axial-flow compressor. Development started at Fredric Flader Inc. in 1947, with the first examples being delivered in 1949. However, these delivered far lower power than predicted. Improved models followed in early 1952 that met the performance requirements, but demonstrated very poor reliability. When small engines from other companies became available, the J55 project was cancelled in 1952.".
- Flader_J55 wikiPageExternalLink books?id=V0SnFt8JGokC&pg=PA46.
- Flader_J55 wikiPageExternalLink 1951%20-%200909.html.
- Flader_J55 wikiPageID "26539964".
- Flader_J55 wikiPageRevisionID "532602679".
- Flader_J55 firstRun "1948".
- Flader_J55 hasPhotoCollection Flader_J55.
- Flader_J55 manufacturer Flader_J55.
- Flader_J55 nationalOrigin United_States.
- Flader_J55 type Turbojet.
- Flader_J55 subject Category:Abandoned_military_aircraft_engine_projects_of_the_United_States.
- Flader_J55 subject Category:Turbojet_engines_1940–1949.
- Flader_J55 comment "The Flader J55, also known as the 124 within the company, was a small turbojet engine notable for its use of a supersonic axial-flow compressor. Development started at Fredric Flader Inc. in 1947, with the first examples being delivered in 1949. However, these delivered far lower power than predicted. Improved models followed in early 1952 that met the performance requirements, but demonstrated very poor reliability.".
- Flader_J55 label "Flader J55".
- Flader_J55 sameAs m.0bh8h1s.
- Flader_J55 sameAs Q5456599.
- Flader_J55 sameAs Q5456599.
- Flader_J55 wasDerivedFrom Flader_J55?oldid=532602679.
- Flader_J55 isPrimaryTopicOf Flader_J55.