Williams J400
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| J400 / WR2 / WR24 | |
|---|---|
| Type | Turbojet |
| National origin | United States |
| Manufacturer | Williams International |
| First run | 1960s |
| Major applications | Canadair CL-89 BQM-74 Chukar |
The Williams International/Rolls-Royce J400 is a small turbojet engine jointly created by Williams International and Rolls-Royce to power target drones.
Design
The J400 is a single-shaft, centrifugal/centrifugal-axial flow turbojet engine.There are two versions of the J400, the WR2 which yields 125 lbst, and the more powerful WR24, which yields 190-240 pounds of thrust.[1][2]
Applications
References
- ^ https://www.forecastinternational.com/archive/disp_pdf.cfm?DACH_RECNO=1191
- ^ Leyes, Richard A.; Fleming, William A. (1999). The history of North American small gas turbine aircraft engines Chapter 10. Washington D.C.: AIAA /Smithsonian Institution. ISBN 1-56347-332-1.
- ^ http://www.designation-systems.net/dusrm/m-74.html
| This article, Williams J400, has recently been created via the Articles for creation process. Please check to see if the reviewer has accidentally left this template after accepting the draft and take appropriate action as necessary.
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