124:
ordered that the S-18 be developed into an operational engine with a thrust of 15.5 kN (3,500 lbf). The TR-1 was developed in early 1946 and had its first static run on 9 August. It was tested in the air on a pylon fitted to a
116:
In May 1944 Lyulka was ordered to begin development of a turbojet with a thrust of 12.3 kN (2,800 lbf). He demonstrated an eight-stage
552:
495:
468:
350:
444:
Turbojet
History and Development 1930-1960 Volume 2:USSR, USA, Japan, France, Canada, Sweden, Switzerland, Italy and Hungary
451:
432:
413:
644:
488:
266:
144:
136:
649:
121:
481:
143:. Lyulka further developed the engine into the TR-1A of 20.5 kN (4,600 lbf) of thrust, but its
322:
139:
than designed. Its failure led directly to the cancellation of the first Soviet jet bomber, the
354:
275:
166:
8:
177:
76:
473:
447:
428:
409:
590:
575:
310:
117:
624:
511:
300:
305:
161:
156:
140:
80:
68:
638:
129:
97:
606:
585:
580:
570:
537:
401:
400:
172:
105:
72:
547:
532:
527:
508:
126:
192:
Gordon, OKB Ilyushin: A History of the Design Bureau and its
Aircraft.
600:
135:
The TR-1 was not a success, proving to have less thrust and a higher
619:
562:
519:
205:
93:
295:
240:
504:
257:
101:
48:
406:
OKB Ilyushin: A History of the Design Bureau and its
Aircraft
120:
engine in March 1945 called the S-18. In early 1946 the
503:
427:(2 ed.). Wellingborough: Patrick Stephens Ltd.
636:
489:
446:(1st ed.). Ramsbury: The Crowood Press.
104:design bureau. It was the first indigenous
496:
482:
196:
404:; Komissarov, Dmitriy and Sergey (2004).
382:
380:
183:
147:was very high and it too was cancelled.
422:
637:
377:
271:129 - 137 kg/kN·h (1.27-1.35 lb/lbf·h)
477:
16:1940s Soviet turbojet aircraft engine
345:
343:
441:
425:World Encyclopaedia of Aero Engines
13:
14:
661:
462:
340:
150:
368:
249:
111:
1:
351:"The USSR into the world Jet"
328:
262:12.8 kN (2,900 lbf)
227:
7:
284:
10:
666:
613:
599:
561:
518:
267:Specific fuel consumption
145:specific fuel consumption
137:specific fuel consumption
21:
469:Early Lyulka jet engines
442:Kay, Anthony L. (2007).
323:List of aircraft engines
645:Lyulka aircraft engines
197:General characteristics
132:piston-engined bomber.
650:1940s turbojet engines
423:Gunston, Bill (1959).
276:Thrust-to-weight ratio
236:eight-stage axial-flow
167:Mikoyan-Gurevich MiG-9
408:. London: Ian Allan.
184:Specifications (TR-1)
122:Council of Ministers
100:and produced by his
169:I-305 (izdeliye FT)
386:Gunston pp. 99–100
290:Comparable engines
64:Major applications
632:
631:
614:Joint development
223:885 kg (1,951 lb)
86:
85:
657:
512:aircraft engines
498:
491:
484:
475:
474:
457:
438:
419:
387:
384:
375:
372:
366:
365:
363:
362:
353:. Archived from
347:
311:Junkers Jumo 004
65:
37:
19:
18:
665:
664:
660:
659:
658:
656:
655:
654:
635:
634:
633:
628:
609:
595:
557:
514:
502:
465:
460:
454:
435:
416:
391:
390:
385:
378:
373:
369:
360:
358:
349:
348:
341:
331:
301:Heinkel HeS 011
287:
252:
230:
199:
186:
153:
114:
79:
75:
71:
63:
36:National origin
35:
17:
12:
11:
5:
663:
653:
652:
647:
630:
629:
617:
615:
611:
610:
605:
603:
597:
596:
594:
593:
588:
583:
578:
573:
567:
565:
559:
558:
556:
555:
550:
545:
540:
535:
530:
524:
522:
516:
515:
501:
500:
493:
486:
478:
472:
471:
464:
463:External links
461:
459:
458:
453:978-1861269393
452:
439:
433:
420:
414:
397:
396:
395:
389:
388:
376:
374:Gordon, p. 112
367:
338:
337:
336:
335:
330:
327:
326:
325:
314:
313:
308:
306:Heinkel HeS 30
303:
298:
286:
283:
282:
281:
272:
263:
251:
248:
247:
246:
237:
229:
226:
225:
224:
218:
213:
208:
198:
195:
185:
182:
181:
180:
175:
170:
164:
162:Ilyushin Il-22
159:
157:Alekseyev I-21
152:
149:
141:Ilyushin Il-22
113:
110:
84:
83:
81:Alekseyev I-21
69:Ilyushin Il-22
66:
60:
59:
58:9 August 1946
56:
52:
51:
46:
42:
41:
38:
32:
31:
28:
24:
23:
15:
9:
6:
4:
3:
2:
662:
651:
648:
646:
643:
642:
640:
626:
623:
621:
616:
612:
608:
604:
602:
598:
592:
589:
587:
584:
582:
579:
577:
574:
572:
569:
568:
566:
564:
560:
554:
551:
549:
546:
544:
541:
539:
536:
534:
531:
529:
526:
525:
523:
521:
517:
513:
510:
506:
499:
494:
492:
487:
485:
480:
479:
476:
470:
467:
466:
455:
449:
445:
440:
436:
434:1-85260-163-9
430:
426:
421:
417:
415:1-85780-187-3
411:
407:
403:
402:Gordon, Yefim
399:
398:
393:
392:
383:
381:
371:
357:on 2011-07-06
356:
352:
346:
344:
339:
333:
332:
324:
321:
320:
319:
318:
317:Related lists
312:
309:
307:
304:
302:
299:
297:
294:
293:
292:
291:
279:
277:
273:
270:
268:
264:
261:
259:
254:
253:
244:
242:
238:
235:
232:
231:
222:
219:
217:
214:
212:
209:
207:
204:
201:
200:
194:
193:
190:
179:
176:
174:
171:
168:
165:
163:
160:
158:
155:
154:
148:
146:
142:
138:
133:
131:
130:B-25 Mitchell
128:
123:
119:
109:
107:
103:
99:
98:Arkhip Lyulka
95:
91:
82:
78:
74:
70:
67:
62:
61:
57:
54:
53:
50:
47:
45:Manufacturer
44:
43:
40:Soviet Union
39:
34:
33:
29:
26:
25:
20:
618:
542:
443:
424:
405:
394:Bibliography
370:
359:. Retrieved
355:the original
316:
315:
289:
288:
274:
265:
255:
245:single stage
239:
233:
220:
215:
210:
202:
191:
188:
187:
178:Sukhoi Su-11
173:Sukhoi Su-10
151:Applications
134:
115:
108:jet engine.
96:designed by
89:
87:
77:Sukhoi Su-11
73:Sukhoi Su-10
250:Performance
234:Compressor:
221:Dry weight:
112:Development
90:Lyulka TR-1
639:Categories
627:(Turbofan)
601:Turboprops
361:2009-09-05
329:References
228:Components
127:Lend-Lease
118:axial-flow
55:First run
563:Turbofans
520:Turbojets
216:Diameter:
189:Data from
30:Turbojet
620:PowerJet
285:See also
256:Maximum
206:Turbojet
94:turbojet
296:BMW 003
241:Turbine
211:Length:
625:SaM146
509:Saturn
505:Lyulka
450:
431:
412:
258:thrust
106:Soviet
102:Lyulka
92:was a
49:Lyulka
607:AL-34
591:AL-55
586:AL-51
581:AL-41
576:AL-32
571:AL-31
538:AL 21
334:Notes
203:Type:
27:Type
22:TR-1
553:TR-7
548:TR-3
543:TR-1
533:AL 7
528:AL 5
507:and
448:ISBN
429:ISBN
410:ISBN
280:1.47
88:The
641::
379:^
342:^
622::
497:e
490:t
483:v
456:.
437:.
418:.
364:.
278::
269::
260::
243::
Text is available under the Creative Commons Attribution-ShareAlike License. Additional terms may apply.