447:, being further developed through several subsequent versions to eventually provide reliable airline service. The Olympus 593 is a prime example of "propulsion and airframe integration". To optimise the performance of the engine when used at speeds from takeoff up to Mach 2 on Concorde, a variable intake and a variable throat nozzle with thrust reversing system were developed. Looking ahead to future supersonic transports, due to noise limits for supersonic transport category airplanes, studies were conducted on ejector suppressors, leading to the conclusion that "a new, low bypass ratio version of the 593 could be suitable for future generations of supersonic transport aircraft".
331:
362:
supervising the first test run and displaying the confidence he had in the design, slammed the throttle to give a surge-free acceleration to maximum power. The thrustmeter showed 10,000 lbf (44 kN). The next development was the BOl.1/2 which produced 9,500 lbf (42 kN) thrust in
December 1950. Examples of the similar BOl.1/2A were constructed for US manufacturer Curtiss-Wright which had bought a licence for developing the engine as the TJ-32 or J67 for the projected
314:. This two-spool design eliminated the need for features such as variable inlet guide vanes (Avon, J79), inlet ramps (J65), variable stators (J79) or compressor bleed (Avon) which were required on single spool compressors with pressure ratios above about 6:1. Without these features an engine could not be started nor run at low speeds without destructive blade vibrations. Nor could they accelerate to high speeds with fast acceleration times ("
42:
322:. The design was progressively modified and the centrifugal HP compressor was replaced by an axial HP compressor. This reduced the diameter of the new engine to the design specification of 40 in (100 cm). The Bristol Type 172 was cancelled though development continued for the Avro Vulcan and other projects.
382:
of 63,668 ft (19,406 m). Fitted with more powerful Mk 102 engines, the
Canberra increased the record to 65,876 ft (20,079 m) in August 1955. The first production Olympus, the Mk 101, entered service in late 1952 at a rated thrust of 11,000 lb, a weight of 3,650 lb, and with a
361:
The BOl.1 first ran on 16 May 1950 and was designed to produce 9,140 lbf (40.7 kN) thrust and to be free from destructive rotating stall on start up to idle speed and to be free from surging on fast accelerations to maximum thrust. The engine started without a problem and Hooker,
338:
The first engine, its development designation being BOl.1 (Bristol
Olympus 1), had six LP compressor stages and eight HP stages, each driven by a single-stage turbine. The combustion system was novel in that ten connected flame tubes were housed within a
3193:
298:
The thrust required of the new engine, then designated B.E.10 (later
Olympus), would initially be 9,000 lbf (40 kN) with growth potential to 12,000 lbf (53 kN). The
2753:
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1213:
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Avro Vulcan Phase 6 (B3): BOl.23, a development of the Mk 301. Different engine configurations, BOl.21, BOl.21/2 and BOl.23, with either reheat or an
374:
936:
221:
in the US as the TJ-32 or J67 (military designation) and the TJ-38 'Zephyr', although none saw use. The
Olympus was also developed with success as
1466:
588:
351:
system. Separate combustion cans would have exceeded the diameter beyond the design limit, and a true annular system was considered too advanced.
1187:
409:
The
Olympus was developed extensively throughout its production run, and the many variants can be described as belonging to four main groups.
1921:
1436:
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and was to be powered by four or six
Bristol engines of 9,000 lbf (40 kN) thrust to the Ministry engine specification TE.1/46.
3202:
1948:
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which first flew with these engines derated to 8,000 lbf (36 kN) thrust in August 1952. In May 1953, this aircraft reached a
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4177:
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551:: Mk 593. Later supersonic airliner design (100 seats). Engine as Mk 591 with zero stage LP compressor and cooled HP turbine.
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229:, which were highly successful. As of 2018, the Olympus remains in service as both a marine and industrial gas turbine.
369:
The engine was by now ready for air testing and the first flight engines, designated
Olympus Mk 99, were fitted into a
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Preserved
Bristol Siddeley Olympus Mk 301 Engine Change Unit (ECU) complete with ancillaries and bulkheads.
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and continued development funding. The engine first ran in 1950 and quickly outperformed its design goals.
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Bristol T198: Mk 591. Early supersonic airliner design (132 seats). The engine was a civilianised BOl.22R.
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Further derivatives of the
Olympus were produced for ship propulsion and land-based power generation.
366:. The somewhat revised BOl.1/2B, ran in December 1951 producing 9,750 lbf (43.4 kN) thrust.
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1998:
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At the end of World War II, the Bristol Engine Company's major effort was the development of the
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1012:
http://webserver.dmt.upm.es/zope/DMT/Members/jmtizon/turbomaquinas/NASA-SP36_extracto.pdf
302:
would be an unheard of 9:1. To achieve this, the initial design used a low-pressure (LP)
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69:
518:, were proposed for this aircraft to provide the required increase in take-off thrust.
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The first reheat variant, the Bristol Siddeley Olympus Mk 320, powered the cancelled
265:
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1314:
502:
Avro 718: BOl.3 The Type 718 was a military transport aircraft with up to 110 seats.
491:
Over the years, the Olympus was proposed for numerous other applications including:
3960:
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1906:
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659:– Mk 202 (Engine is displayed as a Mk 201 but its ECU plate reveals it as a Mk 202)
618:
554:
184:
183:, the engine design's use of twin-spool layout led to continued interest from the
175:
for a jet-powered bomber, powered by four new engines which would be supplied by
3754:
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107:
179:. Although their bomber design was ultimately cancelled in favour of the other
3835:
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3619:
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3342:
3137:
3124:
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41:
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348:
344:
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195:
111:
1219:
1051:"Not Much of an Engineer" Sir Stanley Hooker, The Crowood Press Ltd. 2002,
665:, Doncaster, England - Mk.104 on loan from the Rolls-Royce Heritage Trust.
17:
3860:
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2116:
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1716:
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480:
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257:
180:
162:
150:
57:
1329:
753:
608:
311:
157:, first-run in January 1950. It is best known as the powerplant of the
153:
aircraft engine design, first run in May 1950 and preceded only by the
3147:
1822:
776:
210:
in 1966. Through this period the engine was further developed as the
1138:
https://www.ecfr.gov/current/title-14/chapter-I/subchapter-C/part-36
505:
Avro 739 to OR339 (the requirement that culminated in TSR2): BOl.21R
1454:
1152:
Advanced Olympus for Next Generation Supersonic Transport Aircraft
1125:
Advanced Olympus for Next Generation Supersonic Transport Aircraft
454:
company tested a license-developed version known as the J67 and a
329:
3175:
2735:
1910:
1508:
1495:
653:
Collection (Derby - UK) Mk 101 and Mk 593 and a Marine version.
256:
engines. By the end of 1946, the company had only 10 hours of
279:
submitted a proposal for a medium-range bomber to the same
557:
design to OR339: BOl.14R, BOl.15R. Developed from BOl.6R.
358:
was appointed as Chief Engineer of Bristol Aero Engines.
1318:
Joe Baugher's Encyclopedia of American Military Aircraft
206:
Engines Limited (BSEL), which in turn was taken over by
260:
experience with a small experimental engine called the
1068:"World Encyclopedia of Aero Engines - 5th edition" by
458:
designated TJ-38 Zephyr. Neither design was produced.
1154:. Society of Automotive Engineers, Inc. p. 2267.
1127:. Society of Automotive Engineers, Inc. p. 2266.
4116:
3859:
3515:
3213:
3146:
3119:
3086:
3056:
2981:
2906:
2899:
2840:
2776:
2644:
2616:
2595:
2586:
2368:
2311:
2209:
2115:
2092:
2052:
1956:
1947:
1878:
1845:
1821:
1773:
1715:
1697:
1646:
1582:
1563:
1549:
539:
Bristol T204 to OR339: BOl.22SR (simplified reheat)
190:Initially used in the Vulcan, later versions added
1497:Articles and topics related to Rolls-Royce Olympus
171:The design dates to a November 1946 proposal by
1417:Barnsley, UK: Pen % Sword Aviation, 2012,
1375:. Derby, UK: Rolls-Royce Heritage Trust, 1990.
1320:, 4 December 1999. Retrieved: 16 February 2011.
443:, this was developed during the 1960s into the
275:then in development. In early 1947, the parent
1431:. Marlsborough, UK: Airlife Publishing, 2002.
3187:
2747:
1922:
1520:
1403:. Bishop-Auckland, UK: Pentland Books, 2001.
1282:
1280:
1278:
1276:
1274:
1272:
1270:
1268:
1266:
1264:
1262:
1260:
1258:
1256:
8:
1254:
1252:
1250:
1248:
1246:
1244:
1242:
1240:
1238:
1236:
310:, each being driven by its own single-stage
1182:
1180:
1178:
1176:
1038:
1036:
657:Museum of Science and Industry (Manchester)
27:Supersonic turbojet engine with afterburner
3194:
3180:
3172:
2903:
2754:
2740:
2732:
2592:
1953:
1929:
1915:
1907:
1712:
1560:
1527:
1513:
1505:
1492:
715:127.1 in (10.59 ft; 3.23 m)
428:. These engines were further developed by
904:. Gatwick Aviation Museum. Archived from
880:"The Rolls-Royce Olympus Aircraft Engine"
560:Handley Page HP98: Pathfinder variant of
4173:Rolls-Royce aircraft gas turbine engines
217:Versions of the engine were licensed to
1401:The Vulcan B.Mk2 from a Different Angle
871:
589:Martin/General Dynamics RB-57F Canberra
416:variants were designed and produced by
1212:: CS1 maint: archived copy as title (
1205:
961:: CS1 maint: archived copy as title (
954:
31:
790:0.817 lb/(lbf⋅h) (23.1 g/(kN⋅s))
621:: Development of Mk 555 with aft fan.
7:
1110:"Supersonic Transport (SST) Engines"
721:40 in (3.3 ft; 1.0 m)
343:system: a hybrid of separate flame
198:. Bristol Aero Engines merged with
88:Rolls-Royce Bristol Engine Division
605:: BOl.21 for possible sale to RAF.
334:Gas-flow diagram of Olympus Mk 101
25:
4168:Bristol Siddeley aircraft engines
1488:: YouTube Playlist from AgentJayZ
1389:. London, UK: Grub Street, 2009.
1304:Addendum to Avro Brochure IPB 104
1334:A36 - SAABs atombombare avslöjad
758:HP single stage, LP single stage
439:supersonic strike aircraft. For
84:Bristol Siddeley Engines Limited
40:
1373:Olympus – the first forty years
663:South Yorkshire Aircraft Museum
591:: Mk 701 developed from Mk 301.
585:Hawker P.1129 to OR339: BOl.15R
2369:Rolls-Royce Barnoldswick (RB)
1457:image of Olympus power station
1072:, Sutton Publishing, 2006, p36
826:Rolls-Royce/Snecma Olympus 593
740:axial 6 LP stages, 8 HP stages
567:Handley Page Victor B1: Mk 104
487:Proposed aircraft applications
445:Rolls-Royce/Snecma Olympus 593
401:Rolls-Royce/Snecma Olympus 593
212:Rolls-Royce/Snecma Olympus 593
124:Rolls-Royce/Snecma Olympus 593
1:
727:3,615 lb (1,640 kg)
709:axial flow two-spool turbojet
646:Charlwood Surrey – Two Mk 320
291:. The Bristol design was the
143:) was the world's second two-
3205:gas turbine aircraft engine
1565:Horizontally opposed engines
781:11,000 lbf (49 kN)
670:Specifications (Olympus 101)
397:Rolls-Royce Olympus variants
2587:Aero-derivative industrial
603:Republic F-105 Thunderchief
570:Handley Page Victor Phase 3
495:C104 which led to the C105
4194:
2723:Rolls-Royce Heritage Trust
1450:Rolls-Royce Heritage Trust
821:Rolls-Royce Marine Olympus
697:Bristol Aero Engine School
651:Rolls-Royce Heritage Trust
634:North, Manchester – Mk 101
405:Rolls-Royce Marine Olympus
394:
194:for use in the supersonic
128:Rolls-Royce Marine Olympus
2715:
1551:Bristol Aeroplane Company
1502:
786:Specific fuel consumption
679:"The Operational Olympus"
424:and powered the subsonic
306:and a high-pressure (HP)
283:B.35/46 which led to the
277:Bristol Aeroplane Company
173:Bristol Aeroplane Company
48:
39:
34:
1415:The Avro Type 698 Vulcan
850:List of aircraft engines
354:In 1950, Dr (later Sir)
161:and later models in the
2053:By company designation:
1429:Not Much of an Engineer
1340:issue No. 4, April 1991
1332:quoting Berns, Lennart
1330:Knowledge (XXG) article
1170:25 October 1957, p. 647
1090:Baxter 1990, pp. 22, 24
1030:Baxter 1990, pp. 16, 18
993:Baxter 1990, pp. 13, 18
838:Pratt & Whitney J75
749:cannular 10 flame tubes
701:General characteristics
644:Gatwick Aviation Museum
202:Motors in 1959 to form
155:Pratt & Whitney J57
4178:1950s turbojet engines
4118:Adaptive cycle engines
3203:United States military
984:Baxter 1990, pp. 10–13
815:Bristol Siddeley BS100
795:Thrust-to-weight ratio
594:Gloster P492/3: Mk 591
542:Bristol T205: Mark 551
335:
308:centrifugal compressor
141:Bristol B.E.10 Olympus
2608:Rolls-Royce Meteorite
902:"Rolls-Royce Olympus"
695:Lecture Notes, Vulcan
380:world record altitude
333:
2719:Rolls-Royce Holdings
2652:Alan Arnold Griffith
1463:Good image of Mk 301
1351:Historien om Viggen
1017:20 July 2018 at the
576:Handley Page Pacific
533:Bristol T201: Mk 551
521:Bristol T172: B.E.10
511:Avro 750: 2 x Mk 551
508:Avro 740: 3 x Mk 551
418:Bristol Aero Engines
177:Bristol Aero Engines
80:Bristol Aero Engines
2707:Spirito Mario Viale
1938:Rolls-Royce Limited
1295:Fildes 2012, p. 407
1286:Baxter 1990, p. 172
1230:Fildes 2012, p. 424
1150:Gupta, P.C (1980).
1123:Gupta, P.C (1980).
809:Related development
632:Imperial War Museum
430:Rolls-Royce Limited
326:Initial development
289:Handley Page Victor
137:Rolls-Royce Olympus
3207:designation system
2657:R.W. Harvey-Bailey
2603:Rolls-Royce Meteor
2589:and marine engines
1486:The Mighty Olympus
1476:"Olympian Heights"
1315:"Republic XF-103."
1099:Baxter 1990, p. 32
1081:Baxter 1990, p. 20
1042:Baxter 1990, p. 18
1002:Baxter 1990, p. 13
975:Baxter 2012, p. 20
926:Baxter 2012, p. 16
832:Comparable engines
638:RAF Museum Cosford
626:Engines on display
573:Handley Page HP107
336:
200:Armstrong Siddeley
103:Major applications
4155:
4154:
4149:
4148:
3169:
3168:
3082:
3081:
2729:
2728:
2640:
2639:
2088:
2087:
1904:
1903:
1874:
1873:
1693:
1692:
1461:enginehistory.org
1437:978-1-85310-285-1
1427:Hooker, Stanley.
1423:978 1 84884 284 7
1413:Fildes, David W.
1395:978-1-906502-30-0
1387:Vulcan Test Pilot
1381:978-0-9511710-9-7
908:on 8 January 2017
882:. Air Power World
133:
132:
16:(Redirected from
4185:
3196:
3189:
3182:
3173:
2908:Whirlwind family
2904:
2770:aircraft engines
2756:
2749:
2742:
2733:
2593:
2274:(as Turbo-Union)
2268:(with MAN Turbo)
2247:(with MAN Turbo)
2107:Rolls-Royce RZ.2
1984:Eagle XVI (X-16)
1954:
1931:
1924:
1917:
1908:
1713:
1699:Bristol Siddeley
1561:
1540:Bristol Siddeley
1529:
1522:
1515:
1506:
1493:
1399:Bullman, Craig.
1385:Blackman, Tony.
1358:
1347:
1341:
1327:
1321:
1311:
1305:
1302:
1296:
1293:
1287:
1284:
1231:
1228:
1222:
1217:
1211:
1203:
1201:
1199:
1190:. Archived from
1184:
1171:
1162:
1156:
1155:
1147:
1141:
1135:
1129:
1128:
1120:
1114:
1113:
1106:
1100:
1097:
1091:
1088:
1082:
1079:
1073:
1066:
1060:
1049:
1043:
1040:
1031:
1028:
1022:
1021:p.44 and fig.27a
1009:
1003:
1000:
994:
991:
985:
982:
976:
973:
967:
966:
960:
952:
950:
948:
939:. Archived from
933:
927:
924:
918:
917:
915:
913:
898:
892:
891:
889:
887:
876:
692:
691:on 29 July 2013.
687:. Archived from
422:Bristol Siddeley
304:axial compressor
204:Bristol Siddeley
139:(originally the
120:
104:
66:
44:
32:
21:
4193:
4192:
4188:
4187:
4186:
4184:
4183:
4182:
4158:
4157:
4156:
4151:
4150:
4145:
4112:
3855:
3520:
3511:
3209:
3200:
3170:
3165:
3142:
3115:
3078:
3052:
2977:
2895:
2836:
2772:
2760:
2730:
2725:
2711:
2692:Arthur Rowledge
2636:
2612:
2596:Piston engines:
2588:
2582:
2370:
2364:
2307:
2205:
2111:
2084:
2048:
1943:
1935:
1905:
1900:
1870:
1841:
1817:
1793:Coupled Proteus
1769:
1704:
1689:
1642:
1578:
1553:
1545:
1533:
1498:
1455:Turbine Support
1446:
1441:
1362:
1361:
1348:
1344:
1328:
1324:
1312:
1308:
1303:
1299:
1294:
1290:
1285:
1234:
1229:
1225:
1218:Avro Type List
1204:
1197:
1195:
1194:on 3 March 2016
1188:"Archived copy"
1186:
1185:
1174:
1163:
1159:
1149:
1148:
1144:
1136:
1132:
1122:
1121:
1117:
1108:
1107:
1103:
1098:
1094:
1089:
1085:
1080:
1076:
1067:
1063:
1050:
1046:
1041:
1034:
1029:
1025:
1019:Wayback Machine
1010:
1006:
1001:
997:
992:
988:
983:
979:
974:
970:
953:
946:
944:
943:on 2 April 2015
937:"Archived copy"
935:
934:
930:
925:
921:
911:
909:
900:
899:
895:
885:
883:
878:
877:
873:
858:
806:
771:
734:
703:
677:
672:
628:
598:Republic XF-103
489:
467:
407:
395:Main articles:
393:
328:
268:or core of the
240:
235:
225:and industrial
126:
118:
110:
102:
86:
82:
65:National origin
64:
28:
23:
22:
15:
12:
11:
5:
4191:
4189:
4181:
4180:
4175:
4170:
4160:
4159:
4153:
4152:
4147:
4146:
4144:
4143:
4138:
4133:
4128:
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4114:
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4111:
4110:
4105:
4100:
4095:
4090:
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4063:
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4053:
4048:
4043:
4038:
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4028:
4023:
4018:
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4008:
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3998:
3993:
3988:
3983:
3978:
3973:
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3933:
3928:
3923:
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3871:
3865:
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3833:
3828:
3823:
3818:
3813:
3808:
3802:
3801:
3796:
3791:
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3781:
3775:
3774:
3769:
3763:
3762:
3757:
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3727:
3722:
3717:
3712:
3707:
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3637:
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3582:
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3487:
3481:
3480:
3475:
3470:
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3455:
3450:
3445:
3440:
3435:
3430:
3425:
3420:
3415:
3410:
3405:
3400:
3395:
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3380:
3375:
3370:
3365:
3360:
3355:
3350:
3345:
3340:
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3325:
3320:
3315:
3310:
3305:
3300:
3295:
3290:
3285:
3280:
3275:
3270:
3265:
3260:
3255:
3250:
3245:
3240:
3235:
3230:
3225:
3219:
3217:
3211:
3210:
3201:
3199:
3198:
3191:
3184:
3176:
3167:
3166:
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3163:
3158:
3152:
3150:
3144:
3143:
3141:
3140:
3135:
3129:
3127:
3117:
3116:
3114:
3113:
3108:
3103:
3098:
3092:
3090:
3084:
3083:
3080:
3079:
3077:
3076:
3074:R-2160 Tornado
3071:
3066:
3060:
3058:
3054:
3053:
3051:
3050:
3045:
3040:
3035:
3030:
3025:
3019:
3018:
3013:
3011:Duplex-Cyclone
3008:
3003:
2998:
2993:
2987:
2985:
2983:Cyclone family
2979:
2978:
2976:
2975:
2970:
2965:
2960:
2955:
2950:
2944:
2943:
2938:
2933:
2928:
2923:
2918:
2912:
2910:
2901:
2900:Wright radials
2897:
2896:
2894:
2893:
2888:
2883:
2878:
2873:
2868:
2863:
2858:
2853:
2847:
2845:
2838:
2837:
2835:
2834:
2829:
2824:
2819:
2814:
2809:
2804:
2799:
2794:
2789:
2783:
2781:
2779:inline engines
2774:
2773:
2761:
2759:
2758:
2751:
2744:
2736:
2727:
2726:
2716:
2713:
2712:
2710:
2709:
2704:
2699:
2694:
2689:
2684:
2679:
2677:Adrian Lombard
2674:
2669:
2667:Stanley Hooker
2664:
2659:
2654:
2648:
2646:
2642:
2641:
2638:
2637:
2635:
2634:
2629:
2627:Marine Olympus
2623:
2621:
2614:
2613:
2611:
2610:
2605:
2599:
2597:
2590:
2584:
2583:
2581:
2580:
2575:
2570:
2565:
2560:
2555:
2550:
2545:
2540:
2535:
2530:
2525:
2520:
2515:
2510:
2505:
2500:
2495:
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2465:
2460:
2455:
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2405:
2400:
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2242:
2237:
2232:
2226:
2221:
2215:
2213:
2207:
2206:
2204:
2203:
2198:
2193:
2188:
2183:
2178:
2173:
2168:
2163:
2158:
2153:
2147:
2137:
2132:
2127:
2121:
2119:
2113:
2112:
2110:
2109:
2104:
2098:
2096:
2094:Rocket engines
2090:
2089:
2086:
2085:
2083:
2082:
2077:
2072:
2067:
2062:
2056:
2054:
2050:
2049:
2047:
2046:
2041:
2036:
2031:
2026:
2021:
2016:
2011:
2006:
2001:
1996:
1991:
1986:
1981:
1976:
1971:
1966:
1960:
1958:
1951:
1949:Piston engines
1945:
1944:
1936:
1934:
1933:
1926:
1919:
1911:
1902:
1901:
1899:
1898:
1893:
1891:Stanley Hooker
1888:
1882:
1880:
1876:
1875:
1872:
1871:
1869:
1868:
1863:
1858:
1852:
1850:
1847:Rocket engines
1843:
1842:
1840:
1839:
1834:
1828:
1826:
1819:
1818:
1816:
1815:
1810:
1805:
1800:
1795:
1790:
1784:
1782:
1771:
1770:
1768:
1767:
1762:
1757:
1752:
1747:
1742:
1732:
1726:
1724:
1710:
1707:rocket engines
1695:
1694:
1691:
1690:
1688:
1687:
1682:
1677:
1672:
1667:
1662:
1656:
1654:
1651:radial engines
1644:
1643:
1641:
1640:
1635:
1630:
1625:
1620:
1615:
1610:
1605:
1600:
1595:
1589:
1587:
1584:Radial engines
1580:
1579:
1577:
1576:
1570:
1568:
1558:
1555:Piston engines
1547:
1546:
1534:
1532:
1531:
1524:
1517:
1509:
1503:
1500:
1499:
1496:
1490:
1489:
1483:
1473:
1464:
1458:
1452:
1445:
1444:External links
1442:
1440:
1439:
1425:
1411:
1397:
1383:
1371:Baxter, Alan.
1368:
1367:
1366:
1360:
1359:
1342:
1322:
1313:Baugher, Joe.
1306:
1297:
1288:
1232:
1223:
1172:
1157:
1142:
1130:
1115:
1101:
1092:
1083:
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893:
870:
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867:
863:
862:
857:
854:
853:
852:
841:
840:
829:
828:
823:
818:
817:(Olympus core)
805:
802:
801:
800:
791:
782:
770:
767:
766:
765:
764:AVTUR or AVTAG
759:
750:
741:
733:
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728:
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671:
668:
667:
666:
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654:
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641:
635:
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623:
622:
616:
614:Saab 37 Viggen
611:
606:
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586:
583:
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500:
488:
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473:
466:
463:
452:Curtiss-Wright
392:
389:
387:of 250 hours.
356:Stanley Hooker
327:
324:
300:pressure ratio
264:which was the
239:
236:
234:
231:
219:Curtiss-Wright
214:for Concorde.
131:
130:
121:
119:Developed into
115:
114:
105:
99:
98:
95:
91:
90:
77:
73:
72:
70:United Kingdom
67:
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60:
55:
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26:
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14:
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4119:
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2708:
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2703:
2702:Arthur Rubbra
2700:
2698:
2695:
2693:
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2688:
2687:Harry Ricardo
2685:
2683:
2682:Cyril Lovesey
2680:
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1409:1-85821-899-3
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1221:Avro Heritage
1220:
1215:
1209:
1193:
1189:
1183:
1181:
1179:
1177:
1173:
1169:
1166:
1161:
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1153:
1146:
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1140:, para 36.301
1139:
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1126:
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1105:
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1096:
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1057:9780906393352
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845:
844:Related lists
839:
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816:
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580:Hawker P.1121
578:
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450:The American
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282:
281:specification
278:
274:
271:
267:
266:gas generator
263:
259:
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252:
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245:
237:
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230:
228:
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109:
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78:
76:Manufacturer
75:
74:
71:
68:
63:
62:
59:
56:
53:
52:
47:
43:
38:
33:
30:
19:
3387:
3006:Twin Cyclone
2672:Gordon Lewis
2662:Ernest Hives
2618:Gas turbines
2371:designations
2139:
1989:Eagle (H-24)
1979:Eagle (V-12)
1941:aero engines
1896:Gordon Lewis
1734:
1730:Gyron Junior
1648:Sleeve valve
1543:aero engines
1479:
1467:
1428:
1414:
1400:
1386:
1372:
1365:Bibliography
1354:
1345:
1337:
1333:
1325:
1317:
1309:
1300:
1291:
1226:
1196:. Retrieved
1192:the original
1167:
1160:
1151:
1145:
1133:
1124:
1118:
1104:
1095:
1086:
1077:
1070:Bill Gunston
1064:
1047:
1026:
1007:
998:
989:
980:
971:
945:. Retrieved
941:the original
931:
922:
912:13 September
910:. Retrieved
906:the original
896:
886:13 September
884:. Retrieved
874:
843:
842:
831:
830:
808:
807:
793:
784:
774:
761:
752:
743:
737:
724:
718:
712:
706:
694:
689:the original
682:
674:
673:
619:Vickers VC10
555:de Havilland
549:Bristol T223
545:Bristol T213
536:Bristol T202
527:Bristol T180
524:Bristol T177
490:
465:Applications
460:
449:
434:
411:
408:
373:
368:
360:
353:
337:
297:
241:
227:gas turbines
216:
189:
185:Air Ministry
170:
140:
136:
134:
29:
3522:Turboshafts
3125:turboshafts
2812:T-4 Tornado
2807:T-3 Tornado
2802:T-2 Tornado
2797:T-1 Tornado
2792:Gipsy L-320
2697:Henry Royce
2632:Marine Spey
2317:Turboshafts
2150:Olympus 593
1779:Turboshafts
1709:(1959-1966)
1702:gas turbine
1557:(1920-1956)
1472:of BOl.1/2A
769:Performance
738:Compressor:
725:Dry weight:
471:Avro Vulcan
426:Avro Vulcan
347:and a true
318:") without
285:Avro Vulcan
208:Rolls-Royce
159:Avro Vulcan
108:Avro Vulcan
4162:Categories
3836:LHTEC T800
3517:Turboprops
3121:Turboprops
3016:Cyclone 22
2313:Turboprops
1886:Roy Fedden
1775:Turboprops
1198:28 October
856:References
762:Fuel type:
745:Combustors
732:Components
497:Avro Arrow
414:non-reheat
233:Background
148:axial-flow
94:First run
18:Wright J67
3861:Turbofans
3215:Turbojets
3088:Turbojets
2996:Cyclone 9
2991:Cyclone 7
2841:Lawrance
2717:See also
2645:Designers
2211:Turbofans
2117:Turbojets
2034:Peregrine
1879:Designers
1721:Turbofans
1717:Turbojets
1665:Centaurus
1357:2005 No 4
1338:Flygrevyn
866:Citations
719:Diameter:
675:Data from
582:: BOl.21R
476:BAC TSR-2
456:turboprop
437:BAC TSR-2
273:turboprop
248:Centaurus
196:BAC TSR-2
181:V bombers
112:BAC TSR-2
3841:APW T800
3659:variants
3064:L-3 Gale
2767:Lawrance
2488:RB168-62
2251:RB168-62
2144:variants
1957:By name:
1739:variants
1670:Hercules
1208:cite web
1015:Archived
957:cite web
947:22 March
804:See also
775:Maximum
640:– Mk 320
499:: BOl.3"
481:Concorde
441:Concorde
412:Initial
391:Variants
371:Canberra
341:cannular
316:spool up
293:Type 172
258:turbojet
244:Hercules
163:Concorde
151:turbojet
58:Turbojet
35:Olympus
3657: (
3148:Ramjets
3001:Cyclone
2843:radials
2827:IV-1560
2822:IV-1460
2777:Wright
2240:Pegasus
2201:Welland
2142: (
2140:Olympus
2130:Derwent
2044:Vulture
2029:Pennine
2019:Kestrel
2009:Griffon
2004:Goshawk
1964:Buzzard
1866:Stentor
1823:Ramjets
1813:Theseus
1808:Proteus
1760:Phoebus
1750:Pegasus
1745:Orpheus
1737: (
1735:Olympus
1680:Perseus
1633:Phoenix
1628:Pegasus
1618:Neptune
1613:Mercury
1608:Lucifer
1603:Jupiter
1536:Bristol
1482:article
1470:cutaway
1059:, p.142
754:Turbine
713:Length:
609:Saab 36
516:aft fan
349:annular
312:turbine
270:Proteus
262:Phoebus
238:Origins
3069:R-1200
3057:Others
3048:R-4090
3043:R-3350
3038:R-2600
3033:R-1820
3028:R-1750
3023:R-1300
2973:R-1670
2968:R-1510
2832:V-1950
2763:Wright
2533:RB.193
2473:RB.162
2345:Nimbus
2266:RB.193
2256:RB.175
2235:Medway
2224:Conway
2191:Thames
2171:RB.162
2166:RB.145
2161:RB.108
2156:RB.106
2080:Type R
2075:Type F
2070:Type G
2065:Type H
2024:Merlin
1999:Falcon
1969:Condor
1856:BS.605
1798:Nimbus
1788:BS.360
1755:BS.100
1685:Taurus
1660:Aquila
1574:Cherub
1480:Flight
1468:Flight
1435:
1421:
1407:
1393:
1379:
1355:Protec
1168:Flight
1055:
777:thrust
684:Flight
562:Victor
403:, and
254:piston
251:radial
223:marine
192:reheat
4141:XA103
4136:XA102
4131:XA101
4126:XA100
3996:YF120
3473:YJ101
2963:R-975
2958:R-790
2953:R-760
2948:R-540
2941:J-6-9
2936:J-6-7
2931:J-6-5
2817:V-720
2578:RB508
2573:RB410
2568:RB235
2563:RB220
2558:RB211
2553:RB203
2548:RB207
2543:RB202
2538:RB199
2528:RB183
2523:RB181
2518:RB178
2513:RB177
2508:RB176
2503:RB175
2498:RB174
2493:RB172
2483:RB168
2478:RB163
2468:RB153
2463:RB146
2458:RB145
2453:RB142
2448:RB141
2443:RB140
2438:RB109
2433:RB108
2428:RB106
2355:Tweed
2350:Trent
2340:Gnome
2325:Clyde
2293:RB235
2288:RB220
2283:RB211
2278:RB202
2272:RB199
2261:RB178
2245:RB153
2219:Adour
2196:Viper
2176:RB176
2102:Larch
1974:Crecy
1861:Gamma
1803:Orion
1765:Viper
1675:Orion
1638:Titan
1623:Orion
1598:Hydra
1593:Draco
1478:1961
1165:Arrow
861:Notes
707:Type:
375:WD952
364:F-102
320:surge
145:spool
97:1950
54:Type
4108:F415
4103:F414
4098:F412
4093:F408
4088:F405
4083:F404
4078:F402
4073:F401
4068:F400
4061:F138
4056:F137
4051:F136
4046:F135
4041:F130
4036:F129
4031:F128
4026:F127
4021:F126
4016:F125
4011:F124
4006:F122
4001:F121
3991:F119
3986:F118
3981:F117
3976:F113
3971:F112
3966:F110
3961:F109
3956:F108
3951:F107
3946:F106
3941:F105
3936:F104
3931:F103
3926:F102
3921:F101
3916:F100
3909:TF41
3904:TF39
3899:TF37
3894:TF35
3889:TF34
3884:TF33
3879:TF32
3874:TF31
3869:TF30
3851:T901
3846:T900
3831:T708
3826:T706
3821:T703
3816:T702
3811:T701
3806:T700
3799:T408
3794:T407
3789:T406
3784:T405
3779:T400
3772:T101
3767:T100
3507:J700
3500:J403
3495:J402
3490:J401
3485:J400
3478:J102
3468:J100
3448:YJ93
3318:XJ49
3278:XJ41
3263:XJ38
3161:RJ55
3156:RJ47
2765:and
2721:and
2423:RB93
2418:RB82
2413:RB80
2408:RB53
2403:RB50
2398:RB44
2393:RB41
2388:RB39
2383:RB37
2378:RB23
2360:Tyne
2330:Dart
2298:Spey
2229:M45H
2181:Soar
2135:Nene
2125:Avon
2060:PV12
2014:Hawk
1837:Odin
1832:Thor
1705:and
1433:ISBN
1419:ISBN
1405:ISBN
1391:ISBN
1377:ISBN
1214:link
1200:2011
1053:ISBN
963:link
949:2015
914:2016
888:2016
799:3.04
693:and
649:The
420:and
345:cans
287:and
246:and
135:The
3760:T80
3755:T78
3750:T76
3745:T74
3740:T73
3735:T72
3730:T71
3725:T70
3720:T69
3715:T68
3710:T67
3705:T66
3700:T65
3695:T64
3690:T63
3685:T62
3680:T61
3675:T60
3670:T58
3665:T57
3655:T56
3650:T55
3645:T54
3640:T53
3635:T52
3630:T51
3625:T50
3620:T49
3615:T48
3610:T47
3605:T46
3600:T45
3595:T44
3590:T43
3585:T42
3580:T41
3575:T40
3570:T39
3565:T38
3560:T37
3555:T36
3550:T35
3545:T34
3540:T33
3535:T31
3530:T30
3463:J99
3458:J97
3453:J95
3443:J91
3438:J89
3433:J87
3428:J85
3423:J83
3418:J81
3413:J79
3408:J75
3403:J73
3398:J71
3393:J69
3388:J67
3383:J65
3378:J63
3373:J61
3368:J60
3363:J59
3358:J58
3353:J57
3348:J56
3343:J55
3338:J54
3333:J53
3328:J52
3323:J51
3313:J48
3308:J47
3303:J46
3298:J45
3293:J44
3288:J43
3283:J42
3273:J40
3268:J39
3258:J37
3253:J36
3248:J35
3243:J34
3238:J33
3233:J32
3228:J31
3223:J30
3138:T49
3133:T35
3111:J67
3106:J65
3101:J61
3096:J59
2926:J-5
2921:J-4
2916:J-3
2891:L-5
2886:L-4
2881:L-3
2876:L-2
2871:L-1
2866:J-2
2861:J-1
2856:C-2
2851:A-3
2335:Gem
2186:Tay
2039:"R"
1994:Exe
385:TBO
166:SST
4164::
1777:/
1719:/
1538:/
1336:,
1235:^
1210:}}
1206:{{
1175:^
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