26:
164:
1097:
818:
639:
1107:
1102:
564:
811:
1092:
632:
477:
608:
408:
804:
625:
518:
205:(a.k.a. SNECMA Renault 12T) Refined version of the 12S with new pistons, cylinders and revised induction system.
535:
243:
137:
439:
450 kW (600 hp) at 3,300 rpm / 1,325 mmHg (52.2 inHg) +5.0 kg (11.1 lb) boost
841:
901:
896:
891:
881:
492:
846:
220:
659:
886:
1001:
876:
323:
237:
785:
762:
757:
742:
1061:
1041:
1036:
1031:
1026:
1021:
1006:
931:
926:
921:
916:
911:
727:
991:
986:
981:
971:
966:
961:
956:
936:
604:
560:
468:
248:
70:
851:
772:
692:
687:
273:
830:
651:
314:
44:
143:
Following the end of World War II, Renault continued to manufacture the engine as the
1086:
996:
871:
866:
861:
856:
648:
459:
386:
1x
Bronzavia 92-195A1 updraught carburetor with automatic boost and altitude control.
305:
268:
263:
133:
105:
54:
1016:
780:
747:
707:
682:
677:
523:
375:
253:
186:
176:
121:
109:
92:
1046:
1011:
906:
737:
732:
722:
702:
672:
667:
258:
232:
66:
25:
1071:
1066:
976:
951:
946:
941:
717:
712:
697:
366:
350:
584:(11th ed.). London: Sir Isaac Pitman & Sons Ltd. pp. 296–297.
163:
559:(2nd ed.). Cambridge, England: Patrick Stephens Limited. p. 16.
199:(a.k.a. SNECMA Renault 12S) Designation change on the formation of SNECMA.
617:
211:
827:
796:
125:
451:
260 kW (350 hp) at 3,100 rpm at 2,600 m (8,500 ft)
445:
330 kW (440 hp) at 3,250 rpm at 2,400 m (7,900 ft)
190:
148:
41:
147:. After the merger of the French aircraft engine manufacturers into
162:
129:
500:
371:
One exhaust and one inlet valve per cylinder, push-rod operated.
800:
621:
140:. It developed 600 PS (592 hp, 441 kW) at 3,300 rpm
104:
was an air-cooled, inverted-V12 aircraft engine developed by
120:
The As 411 was a refined and more powerful version of the
380:
Gear driven centrifugal supercharger, 9.25:1 drive ratio.
151:
in 1945, production continued under the new designation
771:
658:
812:
633:
416:Air equipment 50-920 electric inertia starter
8:
603:(1995 ed.). New York: Military Press.
175:A refined and more powerful version of the
819:
805:
797:
640:
626:
618:
167:Argus As 411A in Deutsches Museum München
601:Jane's Fighting Aircraft of World War II
488:0.013 kg/kWh (0.022 lb/(hp⋅h))
124:. Most 411 production was undertaken by
547:
398:Pressure fed 3.9 bar (57 psi)
132:, these engines were used to power the
464:37 kW/L (0.82 hp/cu in)
15:
482:0.30 kg/kWh (0.5 lb/(hp⋅h))
7:
1098:Aircraft air-cooled V piston engines
557:World Encyclopaedia of Aero Engines
582:Aircraft engines of the World 1953
301:12-cylinder inverted 60-degree Vee
288:Aircraft engines of the World 1953
14:
497:0.83 kg/kW (1.36 lb/hp)
413:Planetary reduction gear: 0.572:1
24:
599:Bridgman, Leonard, ed. (1989).
328:12 L (730 cu in)
185:Production of the As 411 after
1:
1108:Inverted V12 aircraft engines
1103:1940s aircraft piston engines
503:13.6 bar (197 psi)
580:Wilkinson, Paul H. (1953).
280:Specifications (SNECMA 12S)
1124:
346:992 mm (39.1 in)
334:1,620 mm (64 in)
837:
519:de Havilland Gipsy Twelve
478:Specific fuel consumption
392:100/130 Aviation gasoline
355:369 kg (814 lb)
319:115 mm (4.5 in)
310:105 mm (4.1 in)
32:
23:
18:
536:List of aircraft engines
340:700 mm (28 in)
293:General characteristics
244:Dassault MD 315 Flamant
138:Dassault MD 315 Flamant
33:Preserved Argus As 411
1093:Argus aircraft engines
555:Gunston, Bill (1989).
168:
116:Design and development
493:Power-to-weight ratio
166:
238:Breguet 892 Mercure
513:Comparable engines
169:
108:in Germany during
62:Major applications
1080:
1079:
794:
793:
566:978-1-85260-163-8
469:Compression ratio
249:Focke-Wulf Fw 189
98:
97:
71:Focke-Wulf Fw 189
1115:
852:Renault 50/60 hp
821:
814:
807:
798:
652:aircraft engines
642:
635:
628:
619:
614:
586:
585:
577:
571:
570:
552:
486:Oil consumption:
274:Sud Ouest S.O.93
221:Ratier propeller
136:and the postwar
89:
79:
63:
28:
16:
1123:
1122:
1118:
1117:
1116:
1114:
1113:
1112:
1083:
1082:
1081:
1076:
833:
825:
795:
790:
767:
654:
646:
611:
598:
595:
593:Further reading
590:
589:
579:
578:
574:
567:
554:
553:
549:
544:
510:
429:
423:
402:Cooling system:
362:
295:
282:
229:
161:
118:
87:
77:
69:
61:
45:aircraft engine
12:
11:
5:
1121:
1119:
1111:
1110:
1105:
1100:
1095:
1085:
1084:
1078:
1077:
1075:
1074:
1069:
1064:
1059:
1054:
1049:
1044:
1039:
1034:
1029:
1024:
1019:
1014:
1009:
1004:
999:
994:
989:
984:
979:
974:
969:
964:
959:
954:
949:
944:
939:
934:
929:
924:
919:
914:
909:
904:
899:
894:
889:
884:
879:
874:
869:
864:
859:
854:
849:
844:
838:
835:
834:
826:
824:
823:
816:
809:
801:
792:
791:
789:
788:
783:
777:
775:
769:
768:
766:
765:
760:
755:
750:
745:
740:
735:
730:
725:
720:
715:
710:
705:
700:
695:
690:
685:
680:
675:
670:
664:
662:
660:Piston engines
656:
655:
647:
645:
644:
637:
630:
622:
616:
615:
609:
594:
591:
588:
587:
572:
565:
546:
545:
543:
540:
539:
538:
527:
526:
521:
509:
506:
505:
504:
498:
489:
483:
474:
465:
460:Specific power
455:
454:
453:
452:
449:Cruising, max:
446:
440:
431:
430:
422:
419:
418:
417:
414:
409:Reduction gear
405:
399:
393:
387:
381:
372:
361:
358:
357:
356:
347:
341:
335:
329:
320:
311:
302:
294:
291:
281:
278:
277:
276:
271:
266:
261:
256:
251:
246:
241:
235:
228:
225:
224:
223:
218:
217:SNECMA 12T-312
215:
209:
208:SNECMA 12T-303
206:
203:
200:
197:
194:
183:
180:
173:
160:
157:
117:
114:
96:
95:
90:
88:Developed from
84:
83:
80:
74:
73:
64:
58:
57:
52:
48:
47:
39:
35:
34:
30:
29:
21:
20:
13:
10:
9:
6:
4:
3:
2:
1120:
1109:
1106:
1104:
1101:
1099:
1096:
1094:
1091:
1090:
1088:
1073:
1070:
1068:
1065:
1063:
1060:
1058:
1055:
1053:
1050:
1048:
1045:
1043:
1040:
1038:
1035:
1033:
1030:
1028:
1025:
1023:
1020:
1018:
1015:
1013:
1010:
1008:
1005:
1003:
1000:
998:
995:
993:
990:
988:
985:
983:
980:
978:
975:
973:
970:
968:
965:
963:
960:
958:
955:
953:
950:
948:
945:
943:
940:
938:
935:
933:
930:
928:
925:
923:
920:
918:
915:
913:
910:
908:
905:
903:
900:
898:
895:
893:
890:
888:
885:
883:
880:
878:
875:
873:
870:
868:
867:80 hp Type WS
865:
863:
862:70 hp Type WC
860:
858:
857:70 hp Type WB
855:
853:
850:
848:
845:
843:
840:
839:
836:
832:
829:
822:
817:
815:
810:
808:
803:
802:
799:
787:
784:
782:
779:
778:
776:
774:
770:
764:
761:
759:
756:
754:
751:
749:
746:
744:
741:
739:
736:
734:
731:
729:
726:
724:
721:
719:
716:
714:
711:
709:
706:
704:
701:
699:
696:
694:
691:
689:
686:
684:
681:
679:
676:
674:
671:
669:
666:
665:
663:
661:
657:
653:
650:
643:
638:
636:
631:
629:
624:
623:
620:
612:
606:
602:
597:
596:
592:
583:
576:
573:
568:
562:
558:
551:
548:
541:
537:
534:
533:
532:
531:
530:Related lists
525:
522:
520:
517:
516:
515:
514:
507:
502:
499:
496:
494:
490:
487:
484:
481:
479:
475:
472:
470:
466:
463:
461:
457:
456:
450:
447:
444:
441:
438:
435:
434:
433:
432:
428:
427:Power output:
425:
424:
420:
415:
412:
410:
406:
403:
400:
397:
394:
391:
388:
385:
382:
379:
377:
373:
370:
368:
364:
363:
359:
354:
352:
348:
345:
342:
339:
336:
333:
330:
327:
325:
321:
318:
316:
312:
309:
307:
303:
300:
297:
296:
292:
290:
289:
286:
279:
275:
272:
270:
269:SNCAC NC.2001
267:
265:
264:Siebel Si 204
262:
260:
257:
255:
252:
250:
247:
245:
242:
239:
236:
234:
231:
230:
226:
222:
219:
216:
213:
210:
207:
204:
201:
198:
195:
192:
188:
184:
181:
178:
174:
171:
170:
165:
158:
156:
154:
150:
146:
141:
139:
135:
134:Siebel Si 204
131:
127:
123:
115:
113:
111:
107:
106:Argus Motoren
103:
94:
91:
86:
85:
81:
76:
75:
72:
68:
65:
60:
59:
56:
55:Argus Motoren
53:
51:Manufacturer
50:
49:
46:
43:
40:
37:
36:
31:
27:
22:
17:
1056:
1051:
842:35-40 hp V-4
831:aero engines
752:
600:
581:
575:
556:
550:
529:
528:
524:Ranger V-770
512:
511:
491:
485:
476:
467:
458:
448:
442:
436:
426:
407:
401:
395:
389:
384:Fuel system:
383:
376:Supercharger
374:
365:
349:
343:
337:
331:
324:Displacement
322:
313:
304:
298:
287:
284:
283:
254:Fouga CM.100
227:Applications
187:World War II
177:Argus As 410
152:
144:
142:
128:in occupied
122:Argus As 410
119:
110:World War II
101:
99:
93:Argus As 410
78:Number built
902:265 hp V-12
897:200 hp V-12
892:190 hp V-12
882:120 hp V-12
877:100 hp V-12
421:Performance
396:Oil system:
259:Pilatus P-2
233:Arado Ar 96
182:Renault 12S
145:Renault 12S
67:Arado Ar 96
1087:Categories
693:140/150 hp
688:120/130 hp
610:0517679647
542:References
404:Air-cooled
390:Fuel type:
367:Valvetrain
360:Components
351:Dry weight
202:SNECMA 12T
196:SNECMA 12S
153:SNECMA 12S
1072:Bengali 6
1067:Bengali 4
847:45 hp V-8
773:Pulse jet
437:Take-off:
285:Data from
240:(4 × 12S)
214:propeller
102:Argus 411
508:See also
212:Dassault
159:Variants
828:Renault
443:Normal:
344:Height:
332:Length:
126:Renault
19:As 411
887:160 hp
786:As 044
781:As 014
763:As 413
758:As 412
753:As 411
748:As 410
743:As 402
738:As 401
708:As III
683:115 hp
678:110 hp
607:
563:
338:Width:
315:Stroke
191:France
172:As 411
149:SNECMA
82:2,600
42:Piston
872:90 hp
733:As 17
728:As 16
723:As 10
703:As II
673:70 hp
668:50 hp
649:Argus
473:6.4:1
299:Type:
130:Paris
38:Type
1017:12Fe
718:As 8
713:As 5
698:As I
605:ISBN
561:ISBN
501:BMEP
306:Bore
100:The
1062:18J
1057:12T
1052:12S
1047:12R
1042:12N
1037:12M
1032:12K
1027:12J
1022:12H
1012:12F
1007:12E
1002:12D
997:12A
932:626
927:468
922:456
917:454
912:446
907:438
189:in
1089::
992:9P
987:9C
982:9A
977:8G
972:8C
967:8B
962:8A
957:7A
952:6Q
947:6P
942:4P
937:4B
155:.
112:.
820:e
813:t
806:v
641:e
634:t
627:v
613:.
569:.
495::
480::
471::
462::
411::
378::
369::
353::
326::
317::
308::
193:.
179:.
Text is available under the Creative Commons Attribution-ShareAlike License. Additional terms may apply.
