29:
481:
505:
102:
90:
585:
404:
37:
28:
707:
578:
541:
371:
712:
121:
that was developed in the early 1970s. It is generally described as being in the "third generation" of Soviet
571:
618:
613:
493:
465:. AlAA/ASME/SAE/ASEE 26th Joint Propulsion Conference, July 16–18, 1990. Orlando, Florida. AIAA-90-2761.
428:
463:
The
Development of Aircraft Power Plant Construction in the USSR and the 60th Anniversary of CIAM
217:
389:
350:
605:
495:中国涡喷15A算不算国产航发 曾用于歼10原型机试飞. Sina Military. Edited: 21 March 2018. Retrieved: 12 July 2021.
8:
537:
656:
346:) with boosted afterburner (CSR mode, altitude < 4,000 metres (13,000 ft))
597:
594:
118:
222:
125:
engines which are characterized by high thrust-to-weight ratios and the use of
701:
681:
676:
671:
666:
661:
651:
633:
628:
623:
233:
126:
563:
555:
416:
239:
227:
179:
643:
122:
484:. Janes Aero Engines. Edited: 1 April 2010. Retrieved: 8 September 2010.
178:
Variant with modified gearbox. Used in several export variants of the
168:
Advanced variant that replaced the -300 model on non-export aircraft.
301:
264:
115:
57:
47:
297:
Two-spool Five-stage low pressure, six-stage high pressure (axial)
310:
327:
211:
155:
78:
144:
Original variant. Used in the MiG-23MF and related variants.
380:
96,8 kg/(h·kN) (0.95 lb/(h·lbf)) at maximum military power
192:
Developed version used in late variants of the MiG-23.
536:. Cambridge, England. Patrick Stephens Limited, 1989.
315:Two-stage high pressure, single-stage low pressure
154:Simplified variant of the engine intended for the
202:Chinese reverse-engineered copy of the R-29-300.
699:
383:202,76 kg/(h·kN) (2 lb/(h·lbf)) with afterburner
593:
579:
245:
586:
572:
482:TMKB Soyuz R29-300 (subscription required)
255:
477:
475:
473:
471:
405:Soyuz Scientific Production Association
38:Deutsches Museum Flugwerft Schleissheim
700:
567:
468:
60:, UMPO, MMP Chernyshev, AMNTK Sojuz
36:Tumansky R-29-300 on display at the
534:World Encyclopaedia of Aero Engines
487:
13:
342:112.81 kilonewtons (25,360 lb
14:
724:
549:
335:78.48 kilonewtons (17,640 lb
27:
506:"Turbofan and Turbojet Engines"
205:
498:
455:
446:
394:4.446; 6.119 with afterburner.
319:
1:
434:
288:
284:1,880 kg (4,140 lb)
272:4,953 mm (195.0 in)
439:
7:
398:
132:
10:
729:
525:
365:Turbine inlet temperature:
278:912 mm (35.9 in)
708:Tumansky aircraft engines
642:
604:
372:Specific fuel consumption
246:Specifications (R-29-300)
35:
26:
21:
556:R-29 on leteckemotory.cz
429:List of aircraft engines
461:Sosounov, V.A. (1990).
256:General characteristics
218:Mikoyan-Gurevich MiG-23
713:1970s turbojet engines
390:Thrust-to-weight ratio
351:Overall pressure ratio
236:(Intended application)
214:(Intended application)
559:(in Czech and Slovak)
452:Gunston 1989, p. 168.
339:) full military (dry)
186:Khatchaturov R-35-300
411:Comparable engines
74:Major applications
695:
694:
108:
107:
720:
598:aircraft engines
588:
581:
574:
565:
564:
560:
519:
518:
516:
515:
510:
502:
496:
491:
485:
479:
466:
459:
453:
450:
99:
87:
75:
31:
19:
18:
728:
727:
723:
722:
721:
719:
718:
717:
698:
697:
696:
691:
638:
600:
592:
558:
552:
547:
532:Gunston, Bill.
528:
523:
522:
513:
511:
508:
504:
503:
499:
492:
488:
480:
469:
460:
456:
451:
447:
442:
437:
401:
377:
345:
338:
332:
322:
291:
258:
248:
208:
135:
119:aircraft engine
97:
85:
73:
17:
16:Soviet turbojet
12:
11:
5:
726:
716:
715:
710:
693:
692:
690:
689:
684:
679:
674:
669:
664:
659:
654:
648:
646:
640:
639:
637:
636:
631:
626:
621:
616:
610:
608:
606:Piston engines
602:
601:
591:
590:
583:
576:
568:
562:
561:
551:
550:External links
548:
546:
545:
529:
527:
524:
521:
520:
497:
486:
467:
454:
444:
443:
441:
438:
436:
433:
432:
431:
420:
419:
408:
407:
400:
397:
396:
395:
386:
385:
384:
381:
368:
362:
359:Air mass flow:
356:
347:
343:
340:
336:
333:
321:
318:
317:
316:
307:
298:
290:
287:
286:
285:
279:
273:
267:
257:
254:
247:
244:
243:
242:
237:
231:
225:
223:Mikoyan MiG-27
220:
215:
207:
204:
200:
199:
197:
196:Shenyang WP-15
190:
189:
187:
176:
175:
173:
166:
165:
163:
152:
151:
149:
142:
141:
139:
134:
131:
106:
105:
100:
98:Developed into
94:
93:
88:
86:Developed from
82:
81:
76:
70:
69:
66:
62:
61:
55:
51:
50:
45:
41:
40:
33:
32:
24:
23:
15:
9:
6:
4:
3:
2:
725:
714:
711:
709:
706:
705:
703:
688:
685:
683:
680:
678:
675:
673:
670:
668:
665:
663:
660:
658:
655:
653:
650:
649:
647:
645:
641:
635:
632:
630:
627:
625:
622:
620:
617:
615:
612:
611:
609:
607:
603:
599:
596:
589:
584:
582:
577:
575:
570:
569:
566:
557:
554:
553:
543:
542:1-85260-163-9
539:
535:
531:
530:
507:
501:
494:
490:
483:
478:
476:
474:
472:
464:
458:
449:
445:
430:
427:
426:
425:
424:
423:Related lists
418:
415:
414:
413:
412:
406:
403:
402:
393:
391:
387:
382:
379:
378:
375:
373:
369:
366:
363:
361:105 kg/s
360:
357:
354:
352:
348:
341:
334:
331:
329:
324:
323:
314:
312:
308:
305:
303:
299:
296:
293:
292:
283:
280:
277:
274:
271:
268:
266:
263:
260:
259:
253:
252:
241:
238:
235:
234:Shenyang J-13
232:
229:
226:
224:
221:
219:
216:
213:
210:
209:
203:
198:
195:
194:
193:
188:
185:
184:
183:
181:
174:
171:
170:
169:
164:
161:
160:
159:
157:
150:
147:
146:
145:
140:
137:
136:
130:
129:air cooling.
128:
124:
120:
117:
113:
112:Tumansky R-29
104:
103:Tumansky R-35
101:
96:
95:
92:
91:Tumansky R-27
89:
84:
83:
80:
77:
72:
71:
67:
64:
63:
59:
56:
54:Manufacturer
53:
52:
49:
46:
43:
42:
39:
34:
30:
25:
20:
686:
644:Gas turbines
533:
512:. Retrieved
500:
489:
462:
457:
448:
422:
421:
417:Lyulka AL-21
410:
409:
388:
370:
364:
358:
349:
325:
309:
300:
294:
281:
275:
269:
261:
250:
249:
240:Sukhoi Su-22
228:Chengdu J-10
206:Applications
201:
191:
180:Sukhoi Su-17
177:
167:
153:
143:
114:is a Soviet
111:
109:
320:Performance
295:Compressor:
282:Dry weight:
230:(Prototype)
123:gas turbine
702:Categories
514:2024-02-10
435:References
302:Combustors
289:Components
172:R-29BS-300
65:First run
440:Citations
276:Diameter:
251:Data from
148:R-29B-300
595:Tumansky
399:See also
367:1,083 °C
326:Maximum
265:Turbojet
138:R-29-300
133:Variants
116:turbojet
58:Tumansky
48:Turbojet
526:Sources
311:Turbine
306:Annular
270:Length:
127:turbine
540:
355:12.9:1
328:thrust
212:IAR 95
162:R-29PN
156:MiG-27
79:MiG-23
657:RD-10
509:(PDF)
262:Type:
68:1972
44:Type
22:R-29
687:R-29
682:R-25
677:R-21
672:R-15
667:R-13
662:R-11
652:RD-9
634:M-90
629:M-88
624:M-87
619:M-86
614:M-85
538:ISBN
110:The
704::
470:^
182:.
158:.
587:e
580:t
573:v
544:.
517:.
392::
376:=
374::
353::
344:f
337:f
330::
313::
304::
Text is available under the Creative Commons Attribution-ShareAlike License. Additional terms may apply.
.jpg)