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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
105:
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
109:
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.
106:
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.
125:
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.
97:. 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)
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Afterburning thrust: 86.3 kN (8,800 kgp / 19,400 lbf)
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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)
401:
Jane, Frederick T. (1975). Taylor, John W. R. (ed.).
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117:turboprop and then later in a big way with the
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405:. New York: Franklin Watts Inc. p. 691.
170:C models and used to upgrade earlier models
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462:. 1976-11-27. p. 1599. Archived from
403:Jane's All The World's Aircraft, 1975-1976
222:
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433:. 1973-11-22. p. 863. Archived from
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618:Manufacturer Specification sheet (pdf)
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574:: CS1 maint: archived copy as title (
530:: CS1 maint: archived copy as title (
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593:"The Dassault Mirage 2000 & 4000"
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391:
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306:95 kN (21,384 lbf) with afterburner
13:
353:2.10(kg/daN.h) maximum afterburner
303:64 kN (14,300 lbf) military thrust
14:
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137:Nozzle of an M53 installed in a
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654:Snecma/Safran aircraft engines
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350:0.90(kg/daN.h) military thrust
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1:
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456:"France's Aircraft Industry"
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907:Low-bypass turbofan engines
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194:Dassault Mirage 2000N/2000D
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336:Turbine inlet temperature:
231:Afterburning single-shaft
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343:Specific fuel consumption
89:engine developed for the
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18:
380:List of aircraft engines
265:8-stage axial compressor
119:Pratt & Whitney JT9D
917:Snecma aircraft engines
246:796 mm (31.33 in) inlet
223:General characteristics
210:Specifications (M53-P2)
912:1970s turbofan engines
833:Europrop International
360:Thrust-to-weight ratio
313:Overall pressure ratio
219:
204:Dassault Mirage F1M-53
141:
101:Design and development
283:2-stage axial turbine
218:Modules of M53 engine
217:
136:
613:Manufacturer website
550:www.flightglobal.com
506:www.flightglobal.com
460:Flight International
431:Flight International
240:5,070 mm (199.60 in)
199:Dassault Mirage 4000
189:Dassault Mirage 2000
91:Dassault Mirage 2000
71:Dassault Mirage 2000
556:on 30 December 2018
512:on 30 December 2018
252:1,515 kg (3,340 lb)
727:Spacecraft engines
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148:- powered initial
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66:Major applications
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787:CFM International
779:Joint development
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466:on 2018-12-30
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412:0-531 03250 7
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374:Related lists
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763:Experimental
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558:. Retrieved
554:the original
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510:the original
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464:the original
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435:the original
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322:Bypass ratio
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183:Applications
163:
145:
139:Mirage 2000B
124:
115:Napier Eland
112:
108:
104:
84:afterburning
79:
77:
859:Olympus 593
851:Rolls-Royce
718:Silvercrest
680:Atar Volant
288:Performance
263:Compressor:
250:Dry weight:
168:Mirage 2000
150:Mirage 2000
93:fighter by
901:Categories
770:Coléoptère
560:12 January
516:12 January
470:2021-05-30
441:2021-05-30
386:References
270:Combustors
257:Components
152:C models
80:SNECMA M53
695:Turbofans
662:Turbojets
427:"Engines"
244:Diameter:
841:TP400-D6
815:PowerJet
744:PPS-1350
675:Atar 101
570:cite web
526:cite web
369:See also
338:1 327 °C
294:Maximum
233:turbofan
129:Variants
87:turbofan
37:Turbofan
754:Vulcain
491:, p.179
332:92 kg/s
279:Turbine
274:annular
238:Length:
882:Larzac
874:Safran
823:SaM146
734:Viking
487:
409:
326:0.36:1
296:thrust
164:M53-P2
95:Snecma
82:is an
59:Snecma
49:France
795:CFM56
749:Vinci
317:9.8:1
229:Type:
146:M53-5
33:Type
864:M45H
805:RISE
800:LEAP
739:HM7B
703:M45G
670:Atar
576:link
562:2022
532:link
518:2022
485:ISBN
407:ISBN
78:The
19:M53
713:M88
708:M53
685:M45
364:6.5
903::
595:.
584:^
572:}}
568:{{
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393:^
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Text is available under the Creative Commons Attribution-ShareAlike License. Additional terms may apply.
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