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153:. The engines were mounted in this fashion to make room for the retracted main undercarriage legs, two on each side attached to the engine nacelles under the wings. The paired main undercarriage legs, side by side, retracted in opposite directions, inboard forwards and outboard rearwards, with the single mainwheels rotating 90 degrees to lie flat under the long jetpipes of the AL-5 engines. To boost takeoff performance, two
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138:, copied the layout of the Il-28, being mounted in the shoulder position at the midpoint of the fuselage. The flying controls consisted of the usual ailerons, elevators and rudder, all fitted with trim tabs for reducing loads on the pilots controls during flight in steady states, as well as "reversible" hydraulically-powered actuators.
105:
project (half the drawings had already been completed). The revised specification was for an aircraft with twice the range and 1 1/2 times the bomb load, with a prototype ready to be submitted for state acceptance trials in July 1952. The
Ilyushin design bureau set about designing two versions of the
118:), with as much as possible common to both aircraft. To meet the schedule for state acceptance trials Ilyushin built only the straight-wing version, fearing that the design, manufacture and flying characteristics of the swept-wing aircraft might cause delays.
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134:, the long fuselage having swept tail surfaces, and a similar arrangement of cockpits for the crew of pilot, navigator and rear gunner. The wing, which had moderate taper but straight
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bottles could be attached to the rear fuselage. Performance was also improved when Lyulka AL-5F (forseerovannyy - afterburning) engines were fitted.
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swept-wing version was designed concurrently, but construction was not started, to ensure that resources were not diverted from the
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2 x 23 mm
Nudelman-Rikhter NR-23 cannon in an Il-K6 turret at the rear of the fuselage.
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engines were fitted in long nacelles forward of the wings, exhausting through long
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proved to have better performance, and was ordered into production as the
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Flight tests and state acceptance trials were successful, with the
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meeting all requirements. Production was not ordered because the
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Gordon, Yefim; Komissarov, Dmitry; Komissarov, Sergey (2004).
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with steel used in highly stressed parts, resembled a large
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during 1951-2, as the result of a directive to redesign the
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Abandoned military aircraft projects of the Soviet Union
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Aircraft of comparable role, configuration, and era
277:, 49.05 kN (11,025 lbf) thrust each
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298:4,845 km (3,011 mi, 2,616 nmi)
149:at the rear of the nacelles, aft of the wing
8:
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292:928 km/h (527 mph, 458 kn)
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333:cannon fixed in the lower port fuselage
422:. Hinkley: Midland. pp. 146–150.
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7:
310:12.25 m/s (2,412.4 ft/min)
255:105 m (1,130.3 sq ft)
243:25.325 m (83 ft 1 in)
106:same aircraft, the straight-wing (
14:
347:
267:52,425 kg (115,597 lb)
249:29 m (95 ft 1 in)
323:3,000 kg of bombs (normal load)
261:26,300 kg (57,991 lb)
304:12,700 m (41,700 ft)
1:
126:The airframe, constructed of
884:Aircraft first flown in 1952
864:1950s Soviet bomber aircraft
448:"Il-46/Il-46S, S.V.Ilyushin"
326:6,000 kg of bombs (overload)
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18:
452:Russian Aviation Museum
228:General characteristics
331:Nudelman-Rikhter NR-23
216:Specifications (Il-46)
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122:Design and development
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194:plan view silhouette
698:Passenger aircraft
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93:was a jet-engined
874:Ilyushin aircraft
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429:978-1-85780-187-3
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454:. Archived from
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97:produced in the
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31:Type of aircraft
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355:Aviation portal
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128:aluminium alloy
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38:National origin
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441:External links
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82:Ilyushin Il-42
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77:Developed from
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53:Design Bureau
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458:on 2007-09-13
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388:Tupolev Tu-16
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383:Tupolev Tu-14
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378:Short Sperrin
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368:Convair XB-46
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265:Gross weight:
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166:Tupolev Tu-88
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151:trailing edge
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136:leading edges
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61:3 March 1952
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58:First flight
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47:Manufacturer
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36:
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29:
26:
23:
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17:
800:Experimental
710:Il-18 (1946)
622:
460:. Retrieved
456:the original
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420:OKB Ilyushin
419:
392:
373:Martin XB-48
361:
360:
315:
313:
307:
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289:
282:
280:
275:Lyul'ka AL-5
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227:
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223:OKB Ilyushin
220:
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161:
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143:Lyul'ka AL-5
140:
125:
115:
107:
90:
88:
67:Number built
283:Performance
271:Powerplant:
858:Categories
766:Il-22 (II)
649:Il-20 (II)
637:Transports
462:2008-11-04
396:References
329:2 x 23 mm
253:Wing area:
112:swept-wing
110:) and the
608:Il-22 (I)
557:Il-20 (I)
247:Wingspan:
221:Data from
190:Ilyushin
879:Twinjets
509:Fighters
503:aircraft
501:Ilyushin
341:See also
316:Armament
199:Variants
147:jetpipes
51:Ilyushin
836:Trainer
689:PAK VTA
581:Bombers
241:Length:
843:Il-103
781:Il-140
761:Il-20M
745:Il-114
740:Il-108
684:Il-276
679:Il-112
674:Il-106
572:Il-102
426:
296:Range:
210:Il-46S
177:Il-46S
116:Il-46S
95:bomber
28:Bomber
19:Il-46
827:Il-26
791:A-100
776:Il-38
771:Il-24
735:Il-96
730:Il-90
725:Il-86
720:Il-62
715:Il-18
705:Il-14
669:Il-80
664:Il-78
659:Il-76
654:Il-32
644:Il-12
628:Il-54
623:Il-46
618:Il-30
613:Il-28
567:Il-42
562:Il-40
552:Il-16
547:Il-10
237:three
235:Crew:
205:Il-46
192:Il-46
181:Il-46
170:Tu-16
162:Il-46
132:Il-28
108:Il-46
103:Il-42
42:USSR
24:Role
822:Il-8
817:Il-1
812:I-21
807:A-60
786:A-50
603:Il-6
598:DB-4
593:Il-4
588:DB-3
542:Il-8
537:Il-2
521:Il-1
516:I-21
424:ISBN
273:2 ×
175:The
155:JATO
141:Two
99:USSR
89:The
860::
450:.
404:^
183:.
172:.
71:1
493:e
486:t
479:v
465:.
432:.
114:(
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