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132:. It had a single-stage low-pressure and an eight-stage high-pressure compressor, powered by a two-stage high-pressure turbine.
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The development of the high-performance single-shaft engine began in 1948. The engine was used in different versions for the
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AM-3M-500, AM-3M-500A: developed further versions with 93.1 kN (20,900 lb
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Chinese copy of the AM-3 with 93.1 kN (20,900 lb
380:. Cambridge, England. Patrick Stephens Limited, 1989.
560:. If you have a source, you can help Knowledge by
155:Version for M-4 with 85.6 kN (19,200 lb
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556:article is missing some (or all) of its
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232:axial-flow, single stage LP, 8-stage HP
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219:3,100 kg (6,800 lb)
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241:14 x can combustion chambers
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207:5,380 mm (212 in)
183:(reproduction of the Tu-16)
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284:Turbine inlet temperature:
213:1,400 mm (55 in)
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291:Specific fuel consumption
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586:Mikulin aircraft engines
339:List of aircraft engines
104:engine developed in the
16:Turbojet aircraft engine
193:General characteristics
581:1950s turbojet engines
300:Thrust-to-weight ratio
276:Overall pressure ratio
116:Design and development
362:Gunston 1989, p. 104.
250:axial-flow, 2-stages
144:first series version
321:Comparable engines
69:Major applications
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562:adding them
255:Performance
230:Compressor:
217:Dry weight:
575:Categories
345:References
237:Combustors
224:Components
507:Turbojets
211:Diameter:
162:AM-3M-200
58:Designer
309:See also
261:Maximum
181:Xian H-6
159:) thrust
136:Variants
102:turbojet
100:) was a
40:Turbojet
423:Mikulin
246:Turbine
205:Length:
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263:thrust
126:Tu-104
552:This
497:AM-47
492:AM-46
487:AM-45
482:AM-44
477:AM-43
472:AM-42
467:AM-39
462:AM-38
457:AM-37
452:AM-35
447:AM-34
350:Notes
286:860°C
199:Type:
152:AM-3D
147:AM-3A
98:RD-3M
36:Type
22:AM-3
530:AM-9
525:AM-5
520:AM-3
515:AM-2
442:M-17
382:ISBN
304:2.81
172:WP-8
141:AM-3
124:and
92:The
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108:by
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