213:
509:
54:
453:
398:(3300 lbf) required. The aircraft made its first flight on 28 May 1947 and also participated in the flypast at Tushino in August. It had a maximum speed of 940 km/h (580 mph) at sea level, but flight testing revealed that it lacked longitudinal stability at high speeds. Modifications of the wing/nacelle
345:
and the aircraft began its state acceptance trials three days later. Flight testing was completed by 25 May 1948 after 136 flights had been completed. It demonstrated a top speed of 885 kilometers per hour (550 mph) at an altitude of 8,000 meters (26,250 ft) and an endurance of one hour and
182:
engines. The design was heavily influenced by captured German jet fighters and it was subsequently redesigned to use a Soviet copy of a German turbojet. The Su-9 was slower than competing Soviet aircraft and it was cancelled as a result. A modified version with different engines and a revised wing
397:
Before the prototype was finished, Sukhoi was ordered to use the Lyulka TR-1 turbojets originally intended for the Su-9. This aircraft was designated the Su-11 and was called
Samolyet KL by the OKB. Each TR-1 developed only 12.7 kN (2,865 lbf) thrust each, rather than the 15 kN
337:
bomber, inexperience with JATO units, and late delivery of RD-10 engines. The first prototype was completed in mid-October and made its first flight on 13 November. The test pilots found the aircraft easy to fly, but the control forces were very high at speed and it lacked enough directional
357:
A two-seat trainer version, the Su-9UT, was planned during 1946, but it too was cancelled. The cockpit for the student would have been positioned ahead of the instructor's cockpit and each would have had a separate canopy. The armament would have been reduced to a pair of 20 millimeters
394:. These changes required that the entire wing be redesigned; the wing spar was bent into an inverted U to accommodate the engines and slotted flaps replaced the simple flaps previously used. The tailplane was given a 5° dihedral to move it out of the engine exhaust.
294:
bottles (11.27 kN (530 lbf) thrust for 8 seconds) mounted on the sides of the fuselage. These reduced the take-off distance by nearly 50 percent and a braking parachute was fitted to reduce the landing distance.
332:
issued an order on 26 February that the manufacturer's flight testing was to begin on 1 November. This goal was not met because the OKB was heavily committed to other projects like the trainer version of the
2483:
258:. The aircraft carried a total of 1,350 kilograms (2,980 lb) of fuel in two bladder tanks, one each ahead and behind the pilot. The low-mounted, straight wing had a single-
426:(unlicensed copies of the Rolls-Royce Derwent) engines with 15.6 kN (3,500 lbf) thrust each. The armament was changed to three 37 mm Nudelman N-37 cannon, while
402:
and lengthening the engine nacelles failed to cure these problems. Coupled with the unavailability of mature TR-1 engines, these problems caused the program to be cancelled.
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1981:
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which increased the aircraft's speed and reduced its dimensions. This consequently increased the take-off and landing speeds so it was equipped with a provision for two
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44 minutes. It had very docile handling qualities with one engine inoperative. The aircraft was recommended for production, but it was significantly slower than the
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1362:
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1384:
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could be reduced if the engine nacelles were mounted in the wing rather than underneath it, and the wing tips were redesigned to use a different
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turbojets, known internally as the
Samolyet or Izdeliye (item or product) K. The ultimate design was very probably influenced by a captured
1355:
414:), was the final attempt to further increase performance of the basic Su-9 design, using wing sections reduced from 11% to 9% thickness/
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was also proposed, but this required major structural changes to accommodate the radar. Neither version made it off the drawing board.
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stability. Enlarging the vertical stabilizer cured this last problem and hydraulic boosters were fitted for the control system.
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17:
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313:. The aircraft carried 100 rounds for each NS-23 and 40 rounds for the N-37. Two 250-kilogram (550 lb) FAB-250
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32:
This article describes the first aircraft to carry the Su-9 designation. For the later supersonic interceptor, see
246:. The pilot was protected by armor plates to his front, an armored seat back and a bulletproof windscreen for the
912:
212:
2446:) • Unknown/no details • Possible error • Unconfirmed
320:
As the TR-1 engines originally intended for the Su-9 were not yet ready for flight testing in late 1945,
362:
autocannon, each with a hundred rounds of ammunition. The armor would have been removed to save weight.
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suggested substituting a pair of Jumo 004 engines and this was approved on 15 December. The full-scale
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bombs could be carried underneath the forward fuselage, but the N-37 had to be dismounted to do so.
235:, but the Su-9 was not a copy of the German aircraft. The Su-9 had an oval cross-section, all-metal
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712:
499:– Su-9 with Klimov RD-500 engines. Night fighter version also proposed. Neither version was built.
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274:. The Su-9 was the first Soviet aircraft to use hydraulic-powered controls. A Soviet copy of the
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The aircraft was revealed to the general public on 3 August 1947 at a flypast at Moscow's
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Another prototype was begun in 1946, but this aircraft was intended to use the
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Sukhoi Su-11 (1947) redirects here. For the later supersonic interceptor, see
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B turbojet, known as the RD-10, was hung under each wing in a streamlined
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that retracted into the fuselage. The Su-9 was designed with a very high
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autocannon. The N-37 could be replaced by a 45-millimeter (1.8 in)
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191:) was a proposal to re-engine the aircraft with Soviet copies of the
713:"Designations of Soviet and Russian Military Aircraft and Missiles."
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Listed in contemporary sources • Bergander list (
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1999:
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354:. The government declined to do so and the program was terminated.
179:
178:. The design began in 1944 and was intended to use Soviet-designed
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The nose housed the armament of one 37-millimeter (1.5 in)
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Abandoned military aircraft projects of the Soviet Union
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tailplanes. The aircraft was also fitted with a pair of
227:) began designing a twin-engined fighter powered by two
187:), but this did not enter production either. The Su-13 (
1377:
328:
was found to be acceptable on 16 February 1946 and the
872:
679:
Aircraft of comparable role, configuration, and era
893:Sukhoi Su-9, −11, −13 at the Sukhoi Company Museum
666:autocannons (200 rounds per gun; 400 rounds total)
2455:
762:
760:
480:– Planned two-seat trainer version, never built.
856:. Hinckley, Leicestershire, UK: Midland, 2002.
382:testing of the Su-9 in September revealed that
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1363:
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1559:for Soviet and Chinese aircraft and missiles
687:– The world's first operational jet fighter.
693:– The first Allied operational jet fighter.
430:could be fitted underneath the wingtips. A
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1534:
1370:
1356:
920:
906:
669:Up to 500 kg (1,100 lb) of bombs
711:Parsch, Andreas and Aleksey V. Martynov.
627:1,200 km (750 mi, 650 nmi)
615:885 km/h (550 mph, 478 kn)
600:, 9 kN (2,000 lbf) thrust each
202:
507:
503:
211:
826:"The Incomplete Guide to Airfoil Usage"
14:
2456:
216:The Su-9 was likely influenced by the
1529:
1351:
901:
817:
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305:and two 23-millimeter (0.91 in)
199:, but neither proposal was accepted.
195:turbojet as well as to modify it for
823:
787:
785:
783:
781:
539:10.546 m (34 ft 7 in)
1378:Soviet straight-winged jet fighters
927:
223:In 1944, the Sukhoi design bureau (
24:
803:
545:11.2 m (36 ft 9 in)
25:
2500:
886:
778:
557:20.2 m (217 sq ft)
551:3.4 m (11 ft 2 in)
718:2008. Retrieved: 19 August 2011.
451:
52:
646:1 × 37 mm (1.457 in)
254:, copied from that used in the
794:
769:
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730:
721:
705:
633:12,800 m (42,000 ft)
581:5,890 kg (12,985 lb)
330:Council of People's Commissars
242:fuselage that housed a single
13:
1:
2469:1940s Soviet fighter aircraft
846:
587:1,350 kg (2,980 lb)
575:4,060 kg (8,951 lb)
27:Experimental fighter aircraft
2489:Aircraft first flown in 1946
653:with 40 rounds or 1 × 45 mm
444:
270:were split and could act as
7:
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390:that significantly reduced
10:
2505:
661:23 mm (0.906 in)
250:. He was provided with an
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519:Early Soviet Jet Fighters
374:-designed version of the
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1557:USAF/DoD reporting names
874:. London: Osprey, 1995.
716:designation-systems.net,
699:
405:
378:RD-10F engine. However,
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1337:List of Sukhoi aircraft
937:Fighters / interceptors
830:m-selig.ae.illinois.edu
736:Gordon, pp. 116, 119–20
524:General characteristics
207:
664:Nudelman-Suranov NS-23
655:Nudelman-Suranov NS-45
513:
348:Mikoyan-Gurevich MiG-9
311:Nudelman-Suranov NS-45
307:Nudelman-Suranov NS-23
284:tricycle undercarriage
220:
203:Design and development
158:'Aircraft K';
1097:Competitive aerobatic
511:
504:Specifications (Su-9)
282:. The aircraft had a
215:
685:Messerschmitt Me 262
266:of 4°20'. The outer
233:Messerschmitt Me 262
218:Messerschmitt Me 262
160:USAF/DoD designation
193:Rolls-Royce Derwent
166:) was an early jet
64:General information
18:Sukhoi Su-11 (1947)
2087:Research/prototype
1813:Research/prototype
1319:T-12 Shturmovik-90
1292:Cancelled projects
800:Gordon, pp. 117–18
775:Gordon, pp. 116–17
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183:became the Su-11 (
58:Sukhoi Su-9 (1946)
2479:Low-wing aircraft
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111:Soviet Air Forces
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276:Junkers Jumo 004
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174:shortly after
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1515:Yak-25 (1947)
1513:
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1324:Sukhoi Shkval
1322:
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1072:S-70 Okhotnik
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868:Gunston, Bill
866:
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862:1-85780-139-3
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648:Nudelman N-37
645:
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579:Gross weight:
577:
574:
573:Empty weight:
571:
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432:night fighter
429:
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424:Klimov RD-500
421:
417:
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401:
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389:
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300:Nudelman N-37
296:
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289:
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277:
273:
269:
265:
262:and a slight
261:
257:
253:
252:ejection seat
249:
248:bubble canopy
245:
241:
238:
237:stressed skin
234:
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226:
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214:
200:
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170:built in the
169:
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55:
50:
45:
41:
35:
30:
19:
2158:Kapustin Yar
1653:
1608:
1565:Type numbers
1476:
1472:Su-11 (1947)
1471:
1466:
1276:Agricultural
1227:Su-17 (1949)
1222:Su-15 (1949)
1216:
1212:Su-11 (1946)
1211:
1201:
1165:Experimental
1156:Superjet 100
871:
853:
833:. Retrieved
829:
819:
796:
771:
750:
741:
732:
723:
715:
707:
696:
678:
677:
638:
636:
630:
624:
618:
612:
605:
603:
590:
584:
578:
572:
560:
554:
548:
542:
536:
530:
523:
521:
516:
515:
494:
492:
486:Samolyet KL)
485:
483:
477:
459:Soviet Union
435:
411:
410:The Su-13, (
409:
396:
376:afterburning
369:
360:Berezin B-20
356:
340:
335:Tupolev Tu-2
322:Pavel Sukhoi
319:
297:
288:wing loading
222:
188:
184:
176:World War II
172:Soviet Union
163:
140:
138:
130:First flight
117:Number built
107:Primary user
88:Manufacturer
82:Soviet Union
40:Sukhoi Su-11
29:
2301:Sary Shagan
1864:Novosibirsk
1823:Caspian Sea
1567:(1947–1955)
1467:Su-9 (1946)
1202:Su-9 (1946)
1192:Su-7 (1944)
606:Performance
591:Powerplant:
495:Samolyet KT
418:ratio and
412:Samolyet KT
380:wind tunnel
229:Lyulka TR-1
189:Samolyot KT
185:Samolyot KL
141:Sukhoi Su-9
34:Sukhoi Su-9
2458:Categories
1144:Transports
847:References
651:autocannon
569:S-10 (11%)
555:Wing area:
428:drop tanks
303:autocannon
272:air brakes
1408:Lavochkin
1385:Alekseyev
621:Mach 0.72
598:turbojets
543:Wingspan:
517:Data from
445:Operators
392:Mach tuck
240:monocoque
149:Самолёт K
102:Cancelled
2474:Twinjets
2267:Plesetsk
2240:Nyonoksa
2089:missiles
2047:Nanchang
2000:Taganrog
1815:aircraft
1487:Yakovlev
1123:Trainers
931:aircraft
835:16 April
674:See also
639:Armament
472:Variants
372:Yakovlev
264:dihedral
180:turbojet
2444:details
2355:Töretam
2097:Barnaul
562:Airfoil
549:Height:
537:Length:
493:Su-13 (
484:Su-11 (
400:fillets
388:airfoil
280:nacelle
244:cockpit
168:fighter
156:
145:Russian
125:History
2170:KY-02
2142:Embi-5
2074:XIAN-A
2037:HARB-A
2029:Harbin
1982:SibNIA
1878:NOVO-C
1874:NOVO-B
1871:NOVO-A
1836:CASP-B
1831:CASP-A
1510:Yak-23
1505:Yak-19
1500:Yak-17
1495:Yak-15
1459:Sukhoi
1431:La-156
1426:La-154
1421:La-152
1416:La-150
1299:KR-860
929:Sukhoi
878:
860:
625:Range:
478:Su-9UT
456:
326:mockup
164:Type 8
99:Status
93:Sukhoi
2429:VA-08
2425:VA-07
2421:VA-06
2418:VA-05
2415:VA-04
2412:VA-03
2409:VA-02
2406:VA-01
2389:TT-09
2385:TT-08
2382:TT-07
2379:TT-06
2375:TT-05
2371:TT-04
2368:TT-03
2365:TT-02
2362:TT-01
2345:SH-11
2341:SH-10
2338:SH-09
2334:SH-08
2330:SH-07
2327:SH-06
2324:SH-05
2320:SH-04
2316:SH-03
2313:SH-02
2309:SH-01
2291:PL-05
2286:PL-04
2282:PL-03
2279:PL-02
2275:PL-01
2257:NE-04
2253:NE-03
2250:NE-02
2247:NE-01
2230:KY-12
2225:KY-11
2221:KY-10
2218:KY-09
2215:KY-08
2211:KY-07
2206:KY-06
2201:KY-05
2196:KY-04
2191:KY-03
2166:KY-01
2149:EM-01
2132:BL-10
2128:BL-09
2125:BL-08
2122:BL-07
2119:BL-06
2116:BL-05
2113:BL-04
2110:BL-03
2107:BL-02
2104:BL-01
2066:Xi'an
2057:NAN-B
2054:NAN-A
2019:TAG-D
2015:TAG-C
2012:TAG-B
2008:TAG-A
1990:SIB-A
1972:RAM-T
1968:RAM-S
1957:RAM-R
1953:RAM-Q
1949:RAM-P
1944:RAM-N
1939:RAM-M
1934:RAM-L
1929:RAM-K
1924:RAM-J
1919:RAM-H
1914:RAM-G
1910:RAM-F
1907:RAM-E
1904:RAM-D
1901:RAM-C
1898:RAM-B
1895:RAM-A
1854:KAZ-A
1846:Kazan
1477:Su-13
1449:MiG-9
1398:I-212
1314:T-60S
1283:Su-38
1267:T-431
1262:T-405
1237:Su-47
1232:Su-37
1217:Su-13
1207:Su-10
1151:Su-80
1135:Su-29
1130:Su-28
1114:Su-31
1109:Su-29
1104:Su-26
1088:Su-12
1067:Su-39
1062:Su-34
1057:Su-25
1052:Su-24
1047:Su-22
1042:Su-20
1037:Su-17
1006:Su-75
1001:Su-57
996:Su-35
991:Su-33
964:Su-30
959:Su-27
954:Su-15
949:Su-11
700:Notes
595:RD-10
567:TsAGI
531:Crew:
439:radar
436:Torii
420:swept
416:chord
406:Su-13
366:Su-11
268:flaps
1888:GFRI
1393:I-21
1309:S-21
1257:T-49
1197:Su-8
1187:Su-6
1182:Su-5
1177:Su-3
1172:Su-1
1032:Su-7
1027:Su-4
1022:Su-2
944:Su-9
876:ISBN
858:ISBN
837:2019
659:2 ×
593:2 ×
512:Su-9
384:drag
350:and
292:JATO
260:spar
208:Su-9
154:lit.
139:The
69:Type
47:Su-9
2184:III
1304:S-6
1252:T-4
1247:T-3
1242:P-1
984:MKM
979:MKK
974:MKI
969:MKA
225:OKB
2460::
2179:II
1962:R2
1804:40
1799:39
1794:38
1789:38
1784:37
1779:36
1774:35
1769:34
1764:33
1759:32
1754:31
1749:30
1744:29
1739:28
1734:27
1729:26
1724:25
1719:24
1714:24
1709:23
1704:22
1699:22
1694:21
1689:20
1684:20
1679:19
1674:19
1669:18
1664:18
1659:17
1654:17
1649:16
1644:15
1639:14
1634:13
1629:12
1624:11
1619:10
870:.
828:.
805:^
780:^
759:^
162::
151:,
147::
2174:I
1614:9
1609:8
1604:7
1599:6
1594:5
1589:4
1584:3
1579:2
1574:1
1549:e
1542:t
1535:v
1371:e
1364:t
1357:v
921:e
914:t
907:v
882:.
864:.
839:.
564::
533:1
497:)
143:(
120:2
20:)
Text is available under the Creative Commons Attribution-ShareAlike License. Additional terms may apply.
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