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28:
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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
2413:
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830:
176:, the development and production of the Tay turbojet was left to Pratt & Whitney. However, Rolls-Royce retained the rights to the Tay outside of the United States.
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fighter aircraft. Concerned that the Nene would not have the potential to cope with future weight growth in improved versions of the
Panther,
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Turbojet
History and Development 1930–1960 Volume 2:USSR, USA, Japan, France, Canada, Sweden, Switzerland, Italy and Hungary
902:
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The Tay/J48 was a thirty percent enlargement of the preceding Nene/J42, and was produced both with and without
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centrifugal-flow turbojet engine under license as the J42 (company designation JT6), for use in the
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design a more powerful engine based on the Nene, which Pratt & Whitney would also produce.
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dry 7,250 lbf (32.2 kN) thrust for take-off; wet 8,500 lbf (38 kN)
264:
6,250 lbf (27.8 kN), 7,000 lbf (31 kN) thrust with water injection
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6,250 lbf (27.8 kN), 7,000 lbf (31 kN) thrust with water injection
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6,350 lbf (28.2 kN), 8,750 lbf (38.9 kN) thrust with afterburning
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6,350 lbf (28.2 kN), 8,750 lbf (38.9 kN) thrust with afterburning
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6,000 lbf (27 kN), 8,000 lbf (36 kN) thrust with afterburning
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Several aircraft types used the J48 engine during the 1950s, including the
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684:. Phoenix Mill, Gloucestershire, England, UK: Sutton Publishing Limited.
607:(15th ed.). London: Sir Isaac Pitman & Sons Ltd. pp. 98–99.
229:
228:
6,000 lbf (27 kN) dry, 8,000 lbf (36 kN) thrust with
180:
640:
Aircraft
Carriers: The world's greatest naval vessels and their aircraft
27:
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1980:
1930:
1925:
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6,250 lbf (27.8 kN), 7,000 lbf (31 kN) thrust with
572:
RAF Flying Review "TECHNICAL GEN" authors: staff, September 1962 p. 59
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2010:
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584:. National Museum of the US Air Force fact sheet. Accessed 2017-07-16
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Data from The
Engines of Pratt & Whitney: A Technical History.
161:, vice president of engineering for P&W's parent company, the
1325:
401:
433:
149:, Pratt & Whitney entered into an agreement to produce the
760:
1352:
413:
421:
pressure spray with scavenge at 40 psi (280 kPa)
622:(13th ed.). London: Sir Isaac Pitman & Sons Ltd.
659:
The
Engines of Pratt & Whitney: A Technical History
554:, U.S. Navy Historical Office. Accessed 2011-01-06.
353:
109.75 in (2,788 mm) without fixed nozzle
663:American Institute of Aeronautics and Astronautics
637:
133:. The Tay/J48 was an enlarged development of the
2459:
526:
524:
682:World Encyclopedia of Aero Engines, 5th Edition
211:used afterburning versions of the J48 engine.
1493:
746:
703:(1st ed.). Ramsbury: The Crowood Press.
587:
538:
536:
521:
319:
726:Pratt & Whitney History page on the J48
397:nine interconnected can combustion chambers
1500:
1486:
753:
739:
611:
596:
533:
453:130 lb/s (59 kg/s) at 11,000 rpm
338:
328:A Pratt & Whitney J48 with afterburner
617:
602:
566:
140:
2468:Rolls-Royce aircraft gas turbine engines
492:Rolls-Royce Nene/Pratt & Whitney J42
323:
288:Commercial engines / company designation
679:
656:
2460:
1469:Pratt & Whitney Canada aeroengines
186:
1481:
734:
282:7,250 lbf (32.2 kN) thrust
276:7,250 lbf (32.2 kN) thrust
698:
638:Bishop, Chris; Chris Chant (2004).
13:
620:Aircraft engines of the World 1955
605:Aircraft engines of the World 1957
462:1.14 lb/(lbf⋅h) (32 g/(kN⋅s))
366:13.9 sq ft (1.29 m)
335:Aircraft engines of the World 1957
129:as a license-built version of the
14:
2489:
2478:Centrifugal-flow turbojet engines
719:
642:. Minneapolis, MN: Zenith Press.
26:
372:2,080 lb (940 kg) dry
292:
1404:Pratt & Whitney Rocketdyne
575:
557:
545:
425:
145:In 1947, at the behest of the
1:
1462:Joint development aeroengines
563:Bishop and Chant 2004, p. 154
509:
376:
347:turbojet with water injection
55:United Kingdom/United States
1511:gas turbine aircraft engine
359:50.5 in (1,280 mm)
7:
618:Wilkinson, Paul H. (1955).
603:Wilkinson, Paul H. (1957).
475:
214:
163:United Aircraft Corporation
137:(Pratt & Whitney J42).
10:
2494:
1399:Pratt & Whitney Canada
385:single-stage double-sided
35:A Pratt & Whitney J48
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458:Specific fuel consumption
320:Specifications (J48-P-8A)
34:
25:
20:
1445:Richard "Dick" Soderberg
941:Free-piston gas turbines
699:Kay, Anthony L. (2007).
504:List of aircraft engines
115:Pratt & Whitney J48
339:General characteristics
309:Lockheed F-94C Starfire
304:Grumman F9F-6/-8 Cougar
205:Lockheed F-94C Starfire
2473:1940s turbojet engines
2424:Adaptive cycle engines
1509:United States military
680:Gunston, Bill (2006).
657:Connors, Jack (2010).
467:Thrust-to-weight ratio
443:Overall pressure ratio
387:centrifugal compressor
329:
141:Design and development
84:Lockheed F-94 Starfire
582:North American YF-93A
487:Rolls-Royce RB.44 Tay
327:
299:Grumman F9F-5 Panther
193:Grumman F9F-5 Panther
117:(company designation
106:Rolls-Royce RB.44 Tay
1440:Frederick Rentschler
661:. Reston. Virginia:
542:Gunston 2006, p.195.
412:aviation kerosene /
314:North American YF-93
209:North American YF-93
125:engine developed by
1363:Aeroderivative gas
762:Pratt & Whitney
481:Related development
199:/F9F-8 Cougar, The
187:Operational history
155:Grumman F9F Panther
127:Pratt & Whitney
76:Grumman F9F Panther
64:Pratt & Whitney
1513:designation system
873:Twin Wasp (R-2000)
868:Twin Wasp (R-1830)
406:single stage axial
330:
147:United States Navy
80:Grumman F-9 Cougar
71:Major applications
2455:
2454:
1475:
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931:XH-3130 (XH-3730)
672:978-1-60086-711-8
649:978-0-7603-2005-1
165:, requested that
111:
110:
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1420:Leonard S. Hobbs
918:H piston engines
883:Twin Wasp Junior
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239:water injection
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908:Yellow Jacket
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691:0-7509-4479-X
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498:Related lists
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364:Frontal area:
362:
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197:Grumman F9F-6
194:
184:
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60:Manufacturer
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33:
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24:
19:
16:
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1392:Subsidiaries
1013:
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631:Bibliography
619:
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344:
332:
331:
293:Applications
230:afterburning
219:
218:
190:
181:afterburning
178:
171:
144:
118:
114:
112:
91:Number built
15:
1828:Turboshafts
1435:Perry Pratt
1243:Turboshafts
898:Wasp Junior
888:Wasp series
878:Twin Wasp E
863:Twin Hornet
848:Double Wasp
552:F9F Panther
426:Performance
419:Oil system:
383:Compressor:
370:Dry weight:
167:Rolls-Royce
2462:Categories
2142:LHTEC T800
1823:Turboprops
1413:Key people
1239:Turboprops
903:Wasp Major
853:Hornet (A)
510:References
410:Fuel type:
393:Combustors
377:Components
159:Luke Hobbs
2167:Turbofans
1521:Turbojets
1466:See also:
1054:Turbofans
959:Turbojets
357:Diameter:
333:Data from
2147:APW T800
1965:variants
1326:Propfans
1309:T800-APW
1164:SuperFan
858:Hornet B
826:R-2180-E
821:R-2180-A
476:See also
432:Maximum
279:J48-P-8A
261:J48-P-6a
215:Variants
123:turbojet
44:Turbojet
1963: (
1378:GG4/FT4
1373:GG3/FT3
1153:RTF-180
1123:PW1000G
402:Turbine
351:Length:
273:J48-P-8
267:J48-P-7
255:J48-P-6
249:J48-P-5
243:J48-P-3
234:J48-P-2
225:J48-P-1
121:) is a
1334:578-DX
1257:JFTD12
1159:STF200
1148:PW6000
1143:PW5000
1138:PW4000
1133:PW2000
1128:PW1120
1093:JTF10A
1062:GP7000
841:R-4360
836:R-2800
831:R-2270
816:R-2060
811:R-2000
806:R-1860
801:R-1830
796:R-1690
791:R-1535
786:R-1340
707:
688:
669:
646:
434:thrust
195:. and
95:4,108
2447:XA103
2442:XA102
2437:XA101
2432:XA100
2302:YF120
1779:YJ101
1251:APW34
1229:XA103
1224:XA101
1170:V2500
1118:JTF22
1113:JTF17
1108:JTF16
1103:JTF14
1098:JT10D
1088:JTF10
781:R-985
515:Notes
447:4.5:1
345:Type:
40:Type
2414:F415
2409:F414
2404:F412
2399:F408
2394:F405
2389:F404
2384:F402
2379:F401
2374:F400
2367:F138
2362:F137
2357:F136
2352:F135
2347:F130
2342:F129
2337:F128
2332:F127
2327:F126
2322:F125
2317:F124
2312:F122
2307:F121
2297:F119
2292:F118
2287:F117
2282:F113
2277:F112
2272:F110
2267:F109
2262:F108
2257:F107
2252:F106
2247:F105
2242:F104
2237:F103
2232:F102
2227:F101
2222:F100
2215:TF41
2210:TF39
2205:TF37
2200:TF35
2195:TF34
2190:TF33
2185:TF32
2180:TF31
2175:TF30
2157:T901
2152:T900
2137:T708
2132:T706
2127:T703
2122:T702
2117:T701
2112:T700
2105:T408
2100:T407
2095:T406
2090:T405
2085:T400
2078:T101
2073:T100
1813:J700
1806:J403
1801:J402
1796:J401
1791:J400
1784:J102
1774:J100
1754:YJ93
1624:XJ49
1584:XJ41
1569:XJ38
1353:RL10
1315:T900
1299:XT57
1289:XT45
1219:TF33
1214:TF30
1203:F401
1198:F135
1193:F119
1188:F117
1183:F105
1178:F100
1083:JT9D
1078:JT8D
1073:JT4D
1068:JT3D
1002:JT12
997:JT11
987:JT8A
972:JT4A
967:JT3C
893:Wasp
705:ISBN
686:ISBN
667:ISBN
644:ISBN
471:3.57
414:JP-4
207:and
174:Avon
113:The
21:J48
2066:T80
2061:T78
2056:T76
2051:T74
2046:T73
2041:T72
2036:T71
2031:T70
2026:T69
2021:T68
2016:T67
2011:T66
2006:T65
2001:T64
1996:T63
1991:T62
1986:T61
1981:T60
1976:T58
1971:T57
1961:T56
1956:T55
1951:T54
1946:T53
1941:T52
1936:T51
1931:T50
1926:T49
1921:T48
1916:T47
1911:T46
1906:T45
1901:T44
1896:T43
1891:T42
1886:T41
1881:T40
1876:T39
1871:T38
1866:T37
1861:T36
1856:T35
1851:T34
1846:T33
1841:T31
1836:T30
1769:J99
1764:J97
1759:J95
1749:J91
1744:J89
1739:J87
1734:J85
1729:J83
1724:J81
1719:J79
1714:J75
1709:J73
1704:J71
1699:J69
1694:J67
1689:J65
1684:J63
1679:J61
1674:J60
1669:J59
1664:J58
1659:J57
1654:J56
1649:J55
1644:J54
1639:J53
1634:J52
1629:J51
1619:J48
1614:J47
1609:J46
1604:J45
1599:J44
1594:J43
1589:J42
1579:J40
1574:J39
1564:J37
1559:J36
1554:J35
1549:J34
1544:J33
1539:J32
1534:J31
1529:J30
1383:FT8
1304:T73
1294:T52
1284:T34
1277:PT5
1272:PT4
1267:PT3
1262:PT2
1208:RM8
1044:J91
1039:J75
1034:J60
1029:J58
1024:J57
1019:J52
1014:J48
1009:J42
992:JT9
982:JT7
977:JT6
949:PT1
203:'s
2464::
1460:†
665:.
535:^
523:^
183:.
1967:)
1825:/
1501:e
1494:t
1487:v
1336:†
1317:†
1311:†
1253:†
1241:/
1210:†
1172:†
1166:†
1155:†
1064:†
754:e
747:t
740:v
713:.
694:.
675:.
652:.
469::
460::
445::
436::
404::
395::
Text is available under the Creative Commons Attribution-ShareAlike License. Additional terms may apply.
