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engine. Modular construction allows sub-assemblies or modules to be changed without the need for full power testing of the engine after replacement. Modules are changed “on condition” by monitoring deteriorating trends in performance and mechanical measurements, such as exhaust gas temperature and
116:
The engine was derived from the Atar series by adding a bypass duct aft of the 3rd compressor stage. The first 3 stages were enlarged to give an LP and HP section on the same shaft. It is a single shaft turbofan, or continuous bleed/bypass turbojet. It was originally called the Super Atar 9K50 and
120:
The engine was designed to have better performance than the latest Atar engines but simpler and less costly than the SNECMA TF 306 turbofan. The fan and HP compressor on the same shaft gave an engine with no restrictions on throttle movements, known as 'carefree handling', during flight.
117:
was designed for sustained flight at Mach 2.5. Flight testing started in July 1973 using a
Caravelle flying test-bed and the engine first went supersonic in a Mirage F.1 test bed at the end of 1974.
136:
The engine is in service in 8 different air forces, powering the whole Mirage 2000 family of airplanes, including the latest Mirage 2000-5 and 2000-9 multirole fighters.
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oil samples, and by visually assessing blade clearances and high temperature distress on internal parts using borescopes.
108:. The engine is in service with different air forces, including the latest Mirage 2000-5 and 2000-9 multirole fighters.
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The
Development Of Jet And Turbine Engines, Bill Gunston, Hayne's Publishing 2006,
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Afterburning thrust: 95.1 kN (9,700 kgp / 21,400 lbf)
169:
Afterburning thrust: 86.3 kN (8,800 kgp / 19,400 lbf)
124:
The engine has a modular construction, first introduced on the
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Dry thrust: 64.7 kN (6,600 kgp / 14,500 lbf)
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Dry thrust: 54.0 kN (5,500 kgp / 12,230 lbf)
412:
Jane, Frederick T. (1975). Taylor, John W. R. (ed.).
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128:turboprop and then later in a big way with the
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416:. New York: Franklin Watts Inc. p. 691.
181:C models and used to upgrade earlier models
8:
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473:. 1976-11-27. p. 1599. Archived from
414:Jane's All The World's Aircraft, 1975-1976
444:. 1973-11-22. p. 863. Archived from
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629:Manufacturer Specification sheet (pdf)
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585:: CS1 maint: archived copy as title (
578:
541:: CS1 maint: archived copy as title (
534:
26:
604:"The Dassault Mirage 2000 & 4000"
7:
317:95 kN (21,384 lbf) with afterburner
364:2.10(kg/daN.h) maximum afterburner
314:64 kN (14,300 lbf) military thrust
25:
148:Nozzle of an M53 installed in a
35:
665:Snecma/Safran aircraft engines
361:0.90(kg/daN.h) military thrust
1:
467:"France's Aircraft Industry"
918:Low-bypass turbofan engines
205:Dassault Mirage 2000N/2000D
944:
347:Turbine inlet temperature:
242:Afterburning single-shaft
354:Specific fuel consumption
100:engine developed for the
34:
29:
391:List of aircraft engines
276:8-stage axial compressor
130:Pratt & Whitney JT9D
928:Snecma aircraft engines
257:796 mm (31.33 in) inlet
234:General characteristics
221:Specifications (M53-P2)
923:1970s turbofan engines
844:Europrop International
371:Thrust-to-weight ratio
324:Overall pressure ratio
230:
215:Dassault Mirage F1M-53
152:
112:Design and development
294:2-stage axial turbine
229:Modules of M53 engine
228:
147:
624:Manufacturer website
561:www.flightglobal.com
517:www.flightglobal.com
471:Flight International
442:Flight International
251:5,070 mm (199.60 in)
210:Dassault Mirage 4000
200:Dassault Mirage 2000
102:Dassault Mirage 2000
82:Dassault Mirage 2000
567:on 30 December 2018
523:on 30 December 2018
263:1,515 kg (3,340 lb)
738:Spacecraft engines
231:
159:- powered initial
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77:Major applications
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798:CFM International
790:Joint development
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16:(Redirected from
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177:- powered later
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385:Related lists
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569:. Retrieved
565:the original
560:
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525:. Retrieved
521:the original
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479:. Retrieved
475:the original
470:
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450:. Retrieved
446:the original
441:
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333:Bypass ratio
331:
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194:Applications
174:
156:
150:Mirage 2000B
135:
126:Napier Eland
123:
119:
115:
95:afterburning
90:
88:
870:Olympus 593
862:Rolls-Royce
729:Silvercrest
691:Atar Volant
299:Performance
274:Compressor:
261:Dry weight:
179:Mirage 2000
161:Mirage 2000
104:fighter by
912:Categories
781:Coléoptère
571:12 January
527:12 January
481:2021-05-30
452:2021-05-30
397:References
281:Combustors
268:Components
163:C models
91:SNECMA M53
18:SNECMA M53
706:Turbofans
673:Turbojets
438:"Engines"
255:Diameter:
852:TP400-D6
826:PowerJet
755:PPS-1350
686:Atar 101
581:cite web
537:cite web
380:See also
349:1 327 °C
305:Maximum
244:turbofan
140:Variants
98:turbofan
48:Turbofan
765:Vulcain
502:, p.179
343:92 kg/s
290:Turbine
285:annular
249:Length:
893:Larzac
885:Safran
834:SaM146
745:Viking
498:
420:
337:0.36:1
307:thrust
175:M53-P2
106:Snecma
93:is an
70:Snecma
60:France
806:CFM56
760:Vinci
328:9.8:1
240:Type:
157:M53-5
44:Type
875:M45H
816:RISE
811:LEAP
750:HM7B
714:M45G
681:Atar
587:link
573:2022
543:link
529:2022
496:ISBN
418:ISBN
89:The
30:M53
724:M88
719:M53
696:M45
375:6.5
914::
606:.
595:^
583:}}
579:{{
559:.
539:}}
535:{{
515:.
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440:.
404:^
657:e
650:t
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373::
356::
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326::
309::
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283::
20:)
Text is available under the Creative Commons Attribution-ShareAlike License. Additional terms may apply.
