The Pratt & Whitney J48 (company designation JT7) is a turbojet engine developed by Pratt & Whitney as a license-built version of the Rolls-Royce Tay. The Tay/J48 was an enlarged development of the Rolls-Royce Nene (Pratt & Whitney J42).
| J48 | |
|---|---|
 |
|
| A Pratt & Whitney J48 | |
| Type | Turbojet |
| Manufacturer | Pratt & Whitney |
| Major applications | Grumman F9F Panther Grumman F-9 Cougar Lockheed F-94 Starfire |
| Number built | 4,108 |
| Developed from | Rolls-Royce RB.44 Tay |
The Pratt & Whitney J48 (company designation JT7) is a turbojet engine developed by Pratt & Whitney as a license-built version of the Rolls-Royce Tay. The Tay/J48 was an enlarged development of the Rolls-Royce Nene (Pratt & Whitney J42).
Contents |
Design and development[edit]
In 1947, at the behest of the United States Navy, Pratt & Whitney entered into an agreement to produce the Rolls-Royce Nene centrifugal-flow turbojet engine under license as the J42 (company designation JT6), for use in the Grumman F9F Panther fighter aircraft.[1] Concerned that the Nene would not have the potential to cope with future weight growth in improved versions of the Panther, Luke Hobbs, vice president of engineering for P&W's parent company, the United Aircraft Corporation, requested that Rolls-Royce design a more powerful engine based on the Nene, which Pratt & Whitney would also produce.
By 1948, Rolls-Royce had designed the Tay turbojet, also a centrifugal-flow design. However, as Rolls-Royce was then developing an improved design with an axial compressor, which would become the Avon, the development and production of the Tay turbojet was left to Pratt & Whitney.[1][2] However, Rolls-Royce retained the rights to the Tay outside of the United States.
The Tay/J48 was a thirty percent enlargement of the preceding Nene/J42, and was produced both with and without afterburning.[2]
Operational history[edit]
Several aircraft types used the J48 engine during the 1950s, including the Grumman F9F-5 Panther.[3] and Grumman F9F-6/F9F-8 Cougar,[4] The U.S. Air Force's Lockheed F-94C Starfire[5] and North American YF-93 used afterburning versions of the J48 engine.[6]
Variants[edit]
Data from: The Engines of Pratt & Whitney: A Technical History[7]
- J48-P-1: 6,000 lbf (26.7 kN), 8,000 lbf (35.6 kN) thrust with afterburning
- J48-P-2: 6,250 lbf (27.8 kN), 7,000 lbf (31.1 kN) thrust with water injection
- J48-P-3: 6,000 lbf (26.7 kN), 8,000 lbf (35.6 kN) thrust with afterburning
- J48-P-5: 6,350 lbf (28.2 kN), 8,750 lbf (38.9 kN) thrust with afterburning
- J48-P-6: 6,250 lbf (27.8 kN), 7,000 lbf (31.1 kN) thrust with water injection
- J48-P-7: 6,350 lbf (28.2 kN), 8,750 lbf (38.9 kN) thrust with afterburning
- J48-P-8: 7,250 lbf (32.2 kN) thrust
- J48-P-8A: 7,250 lbf (32.2 kN) thrust
Applications[edit]
Specifications (J48-P-8A)[edit]
 |
This aircraft engine article is missing some (or all) of its specifications. If you have a source, you can help Wikipedia by adding them. |
Data from The Engines of Pratt & Whitney: A Technical History[7]
General characteristics
- Type: Turbojet
- Length: 202 in (513 cm)
- Diameter: 50 in (127 cm)
- Dry weight: 2,101 lb (953 kg)
Components
- Compressor: Centrifugal compressor
Performance
- Maximum thrust: 7,250 lbf (32.2 kN) thrust
- Power-to-weight ratio:
See also[edit]
- Related development
- Related lists
References[edit]
- Notes
- ^ a b Connors, p.202
- ^ a b Gunston 2006, p.195.
- ^ F9F Panther, U.S. Navy Historical Office. Accessed 2011-01-06.
- ^ Bishop and Chant 2004, p. 154
- ^ RAF Flying Review "TECHNICAL GEN" authors: staff, September 1962 page 59
- ^ North American YF-93A. National Museum of the US Air Force fact sheet. Accessed 2011-01-06
- ^ a b Connors, p.210
- Bibliography
- Bishop, Chris; Chris Chant (2004). Aircraft Carriers: The world's greatest naval vessels and their aircraft. Minneapolis, MN: Zenith Press. ISBN 978-0-7603-2005-1.
- Connors, Jack (2010). The Engines of Pratt & Whitney: A Technical History. Reston. Virginia: American Institute of Aeronautics and Astronautics. ISBN 978-1-60086-711-8.
- Gunston, Bill (2006). World Encyclopedia of Aero Engines, 5th Edition. Phoenix Mill, Gloucestershire, England, UK: Sutton Publishing Limited. ISBN 0-7509-4479-X.
- Kay, Anthony L. (2007). Turbojet History and Development 1930-1960 Volume 2:USSR, USA, Japan, France, Canada, Sweden, Switzerland, Italy and Hungary (1st ed.). Ramsbury: The Crowood Press. ISBN 978-1861269393.
External links[edit]
 |
Wikimedia Commons has media related to: Pratt & Whitney J48 |
|
||||||||||||||||||||||||||||||||||||||
|
|||||||||||
|
||||||||||||||
