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air-launched cruise missile. Although the AGM-137 was cancelled, the F122 was first used for the Taurus KEPD when it was flown aboard that missile in April 2002.
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is a twin-shaft, axial-centrifugal-flow turbofan that is similar to the F107 in configuration but has a maximum thrust of 900 lbf (3.33 to 4.0 kN).
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The history of North
American small gas turbine aircraft engines Chapter 10
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2-stage fan, 2-stage axial IP compressor, 1-stage centrifugal HP compressor
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543:(21st ed.). Washington D.C.: Paul H. Wilkinson. p. 120.
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614:The initial version of this article was based on a
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430 lbf (1.9 kN) Maximum continuous power
598:. Washington D.C.: AIAA /Smithsonian Institution.
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594:Leyes, Richard A.; Fleming, William A. (1999).
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135:. It has been used as the powerplant for the
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555:"Designations Of U.S. Military Aero Engines"
633:National Museum of the USAF F107 fact sheet
479:, and was the powerplant for the cancelled
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638:F107-WR-400_Turbofan_PCS_-_October_1984
360:0.683 lb/lbf/h (69.6 kg/kN/h)
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265:1-stage HP turbine, 2-stage LP turbine
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16:Turbofan engine for cruise missiles
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541:Aircraft engines of the World 1970
204:Aircraft engines of the World 1970
131:. The F107 was designed to propel
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1759:Centrifugal-flow turbojet engines
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36:An F107 engine on display at the
38:San Diego Air & Space Museum
27:
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471:The F122 is used to power the
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186:Bell Aerospace Flying Jet Belt
143:, as well as the experimental
1:
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327:1,400 lbf (6.22 kN)
238:
787:gas turbine aircraft engine
573:"Northrop AGM/MGM-137 TSSAM"
7:
1744:Low-bypass turbofan engines
577:www.designation-systems.net
559:www.designation-systems.net
539:Wilkinson, Paul H. (1970).
503:
461:Williams International F122
283:Pressure system with return
10:
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320:700 lbf (3.1 kN)
313:610 lbf (2.7 kN)
256:Annular combustion chamber
1754:Williams aircraft engines
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356:Specific fuel consumption
35:
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620:Greg Goebel's Vectorsite
510:List of aircraft engines
433:699 (as of August 2014)
228:12 in (300 mm)
222:24 in (610 mm)
373:
234:67 lb (30 kg)
208:General characteristics
1749:1970s turbofan engines
1700:Adaptive cycle engines
785:United States military
467:Design and development
410:Williams International
365:Thrust-to-weight ratio
338:Overall pressure ratio
191:Dynetics Gremlins X-61
129:Williams International
68:Williams International
197:Specifications (WR19)
119:(company designation
176:Kaman KSA-100 SAVER
145:Kaman KSA-100 SAVER
789:designation system
417:Major applications
83:Major applications
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481:AGM-137 TSSAM
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475:air-launched
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452:Williams F415
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1104:Turboshafts
318:F107-WR-402
311:F107-WR-400
288:Performance
281:Oil system:
245:Compressor:
232:Dry weight:
161:AGM-86 ALCM
137:AGM-86 ALCM
88:AGM-86 ALCM
1738:Categories
1418:LHTEC T800
1099:Turboprops
526:References
269:Fuel type:
252:Combustors
239:Components
74:First run
1443:Turbofans
797:Turbojets
685:Turbofans
448:Variants
226:Diameter:
202:Data from
1423:APW T800
1241:variants
504:See also
498:KEPD 350
473:KEPD 350
422:KEPD 350
390:Turbofan
294:Maximum
216:Turbofan
125:turbofan
96:AGM-158B
48:Turbofan
1239: (
261:Turbine
220:Length:
602:
342:13.8:1
296:thrust
139:, and
77:1970s
1723:XA103
1718:XA102
1713:XA101
1708:XA100
1578:YF120
1055:YJ101
386:Type
214:Type:
44:Type
1690:F415
1685:F414
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1670:F405
1665:F404
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1538:F108
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1523:F105
1518:F104
1513:F103
1508:F102
1503:F101
1498:F100
1491:TF41
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