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216:(a.k.a. SNECMA Renault 12T) Refined version of the 12S with new pistons, cylinders and revised induction system.
546:
254:
148:
450:
450 kW (600 hp) at 3,300 rpm / 1,325 mmHg (52.2 inHg) +5.0 kg (11.1 lb) boost
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Following the end of World War II, Renault continued to manufacture the engine as the
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470:
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1x
Bronzavia 92-195A1 updraught carburetor with automatic boost and altitude control.
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595:(11th ed.). London: Sir Isaac Pitman & Sons Ltd. pp. 296–297.
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570:(2nd ed.). Cambridge, England: Patrick Stephens Limited. p. 16.
210:(a.k.a. SNECMA Renault 12S) Designation change on the formation of SNECMA.
628:
222:
838:
807:
136:
462:
260 kW (350 hp) at 3,100 rpm at 2,600 m (8,500 ft)
456:
330 kW (440 hp) at 3,250 rpm at 2,400 m (7,900 ft)
201:
159:
52:
158:. After the merger of the French aircraft engine manufacturers into
173:
140:
511:
382:
One exhaust and one inlet valve per cylinder, push-rod operated.
811:
632:
151:. It developed 600 PS (592 hp, 441 kW) at 3,300 rpm
115:
was an air-cooled, inverted-V12 aircraft engine developed by
131:
The As 411 was a refined and more powerful version of the
391:
Gear driven centrifugal supercharger, 9.25:1 drive ratio.
162:
in 1945, production continued under the new designation
782:
669:
823:
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427:Air equipment 50-920 electric inertia starter
8:
614:(1995 ed.). New York: Military Press.
186:A refined and more powerful version of the
830:
816:
808:
651:
637:
629:
178:Argus As 411A in Deutsches Museum München
612:Jane's Fighting Aircraft of World War II
499:0.013 kg/kWh (0.022 lb/(hp⋅h))
135:. Most 411 production was undertaken by
558:
409:Pressure fed 3.9 bar (57 psi)
143:, these engines were used to power the
475:37 kW/L (0.82 hp/cu in)
26:
493:0.30 kg/kWh (0.5 lb/(hp⋅h))
7:
1109:Aircraft air-cooled V piston engines
568:World Encyclopaedia of Aero Engines
593:Aircraft engines of the World 1953
312:12-cylinder inverted 60-degree Vee
299:Aircraft engines of the World 1953
25:
508:0.83 kg/kW (1.36 lb/hp)
424:Planetary reduction gear: 0.572:1
35:
610:Bridgman, Leonard, ed. (1989).
339:12 L (730 cu in)
196:Production of the As 411 after
1:
1119:Inverted V12 aircraft engines
1114:1940s aircraft piston engines
514:13.6 bar (197 psi)
591:Wilkinson, Paul H. (1953).
291:Specifications (SNECMA 12S)
1135:
357:992 mm (39.1 in)
345:1,620 mm (64 in)
848:
530:de Havilland Gipsy Twelve
489:Specific fuel consumption
403:100/130 Aviation gasoline
366:369 kg (814 lb)
330:115 mm (4.5 in)
321:105 mm (4.1 in)
43:
34:
29:
547:List of aircraft engines
351:700 mm (28 in)
304:General characteristics
255:Dassault MD 315 Flamant
149:Dassault MD 315 Flamant
44:Preserved Argus As 411
1104:Argus aircraft engines
566:Gunston, Bill (1989).
179:
127:Design and development
504:Power-to-weight ratio
177:
249:Breguet 892 Mercure
524:Comparable engines
180:
119:in Germany during
73:Major applications
1091:
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805:
804:
577:978-1-85260-163-8
480:Compression ratio
260:Focke-Wulf Fw 189
109:
108:
82:Focke-Wulf Fw 189
16:(Redirected from
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863:Renault 50/60 hp
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497:Oil consumption:
285:Sud Ouest S.O.93
232:Ratier propeller
147:and the postwar
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604:Further reading
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413:Cooling system:
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671:Piston engines
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471:Specific power
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460:Cruising, max:
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420:Reduction gear
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228:SNECMA 12T-312
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219:SNECMA 12T-303
217:
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99:Developed from
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18:Renault 12S-02
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878:80 hp Type WS
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873:70 hp Type WC
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868:70 hp Type WB
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541:Related lists
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438:Power output:
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280:SNCAC NC.2001
278:
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275:Siebel Si 204
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145:Siebel Si 204
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117:Argus Motoren
114:
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66:Argus Motoren
64:
62:Manufacturer
61:
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57:
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51:
48:
47:
42:
38:
33:
28:
19:
1067:
1062:
853:35-40 hp V-4
842:aero engines
763:
611:
592:
586:
567:
561:
540:
539:
535:Ranger V-770
523:
522:
502:
496:
487:
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469:
459:
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447:
437:
418:
412:
406:
400:
395:Fuel system:
394:
387:Supercharger
385:
376:
360:
354:
348:
342:
335:Displacement
333:
324:
315:
309:
298:
295:
294:
265:Fouga CM.100
238:Applications
198:World War II
188:Argus As 410
163:
155:
153:
139:in occupied
133:Argus As 410
130:
121:World War II
112:
110:
104:Argus As 410
89:Number built
913:265 hp V-12
908:200 hp V-12
903:190 hp V-12
893:120 hp V-12
888:100 hp V-12
432:Performance
407:Oil system:
270:Pilatus P-2
244:Arado Ar 96
193:Renault 12S
156:Renault 12S
78:Arado Ar 96
1098:Categories
704:140/150 hp
699:120/130 hp
621:0517679647
553:References
415:Air-cooled
401:Fuel type:
378:Valvetrain
371:Components
362:Dry weight
213:SNECMA 12T
207:SNECMA 12S
164:SNECMA 12S
1083:Bengali 6
1078:Bengali 4
858:45 hp V-8
784:Pulse jet
448:Take-off:
296:Data from
251:(4 × 12S)
225:propeller
113:Argus 411
519:See also
223:Dassault
170:Variants
839:Renault
454:Normal:
355:Height:
343:Length:
137:Renault
30:As 411
898:160 hp
797:As 044
792:As 014
774:As 413
769:As 412
764:As 411
759:As 410
754:As 402
749:As 401
719:As III
694:115 hp
689:110 hp
618:
574:
349:Width:
326:Stroke
202:France
183:As 411
160:SNECMA
93:2,600
53:Piston
883:90 hp
744:As 17
739:As 16
734:As 10
714:As II
684:70 hp
679:50 hp
660:Argus
484:6.4:1
310:Type:
141:Paris
49:Type
1028:12Fe
729:As 8
724:As 5
709:As I
616:ISBN
572:ISBN
512:BMEP
317:Bore
111:The
1073:18J
1068:12T
1063:12S
1058:12R
1053:12N
1048:12M
1043:12K
1038:12J
1033:12H
1023:12F
1018:12E
1013:12D
1008:12A
943:626
938:468
933:456
928:454
923:446
918:438
200:in
1100::
1003:9P
998:9C
993:9A
988:8G
983:8C
978:8B
973:8A
968:7A
963:6Q
958:6P
953:4P
948:4B
166:.
123:.
831:e
824:t
817:v
652:e
645:t
638:v
624:.
580:.
506::
491::
482::
473::
422::
389::
380::
364::
337::
328::
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204:.
190:.
20:)
Text is available under the Creative Commons Attribution-ShareAlike License. Additional terms may apply.
