Knowledge (XXG)

Antonov An-180

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airliners. Antonov was discussing this aircraft in Soviet aviation publications as early as October 1990, describing the An-180 as a 164-180 passenger plane with a range of 1,300 to 1,600 nautical miles (2,500 to 3,000 kilometres; 1,600 to 1,900 miles) and a per-passenger fuel consumption of 14 to 15
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It was planned to have a number of variants with seating starting at 150–156 passengers, to a larger variant for 200 passengers, and it was also planned to build a combination passenger/freight and an all-freight variant. The cabin is configured to use two aisles, with a seating row containing two
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propfan mounted at the end of each tailplane. Each propfan was to have a coaxial contra-rotating tractor propeller, and the An-180 was also designed with a retractable landing gear with twin nosewheels, and tandem pairs of mainwheels.
26: 183:, with follow-up tests in July to finalize the design, but financial problems delayed the completion of the study as of November 1994. By February 1995, joint manufacturing was expected to begin at the aircraft factories in 979:] (Television production) (in Russian). Interviews with Yakovlev general designer A. Dondukov and Antonov general designer P. V. Balabuyev. Event occurs at 39:42 and 40:51 – via sibnet.ru. 990: 211:, the Ukrainian manufacturer of the D-27. Subsequent attempts to obtain commercial investment failed, though, and by 2004, the An-180 was no longer an Antonov project. 837:"State of change: Ukraine's aerospace industry is shaking off the legacy of the Soviet era with new products, developed since independence, coming onto the market" 1404: 1039: 195:. Because of extreme funding shortfalls from the Ukraine government, however, the development of the An-180 was fully suspended by August 1995. In 1999, 235:
seats each between an aisle and the adjacent windows/cabin walls, and two seats between the two aisles. The undercarriage can store seven LD3-46
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The An-180 was a conventionally designed low-wing cantilever monoplane with a conventional tail unit. The unusual feature was the mounting of an
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3,300 km (2,100 mi, 1,800 nmi) maximum takeoff weight; 1,800 km (1,100 mi; 970 nmi) normal takeoff weight
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of an uncompleted An-180 aircraft remained in storage in a building used for assembly of Antonov's experimental models.
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in a conventional tail configuration. In 1992, Ukraine and China were studying whether to jointly develop the aircraft.
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grams per kilometre (0.79 to 0.85 ounces per mile). The proposed aircraft was introduced to the world at the 1991
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In April 1994, a prototype of the aircraft was tested at the Russian Central Aviation Institute's transonic
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fuselage, but Antonov later modified the design so that the engines were attached to the ends of the
1301: 1265: 742: 707: 1291: 132: 41: 575: 451: 445: 948: 906: 846: 817: 786: 680: 555: 527: 465: 455: 200: 905:(FBIS) (published April 8, 1992). Kryl'ia Rodiny (Wings of the Motherland). pp. 70–73. 754: 719: 641: 496: 236: 184: 526:(FBIS) (published February 1, 1991). Vozdushnyy Transport (Air Transport). pp. 63–64. 693: 409: 376: 156: 495:(FBIS) (published April 28, 1993). Uryadovyy Kuryer (Official Courier). pp. 81–82. 1229: 1214: 1103: 1093: 1088: 1083: 875: 870: 404: 308:
71,700 kg (158,071 lb) normal takeoff weight 67,500 kg (148,812 lb)
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Siruk, Mykola (August 12, 2003). "Ukrainian, Russian planes compete for CIS market".
384: 315: 227: 196: 640:(FBIS) (published November 2, 1992). Tokyo Kyodo. October 31, 1992. pp. 11–12. 1357: 1352: 1347: 1342: 1281: 1250: 1139: 1134: 1129: 1124: 645: 500: 192: 62: 1337: 1332: 1327: 1322: 1317: 1296: 758: 723: 602: 180: 753:(FBIS) (published August 8, 1995). Vechirniy Kyyiv (Evening Kiev). p. 65. 597: 576:"Freighter specialist Antonov broadens focus by developing passenger aircraft" 389: 366: 208: 952: 910: 878:
Ukraine & Baltics. Kiev, Ukraine (published August 15, 2003) – via
850: 821: 790: 559: 531: 715: 664: 469: 25: 947:] (in Russian). No. 5 (published May 1995). 1995. pp. 15–16. 998: 936:[Quick guide to Russian and Ukrainian aircraft and helicopters]. 672: 328: 215: 47: 1048: 879: 318: 136: 128: 66: 44: 659:"Aircraft industry on financial problems". Ukraine: Economic issues. 394: 165: 933:КРАТКИЙ СПРАВОЧНИК ПО РОССИЙСКИМ И УКРАИНСКИМ САМОЛЕТАМ И ВЕРТОЛЕТАМ 1017: 554:. Vol. 148, no. 4501. December 6–12, 1995. p. 60. 203:
were still expected to be built for the An-180, according to the
845:. Vol. 166, no. 4951. Moscow, Russia. pp. 40–41. 1021: 204: 169: 926: 924: 922: 920: 600:[Dreaming is not harmful. Part 2. Project AN-180.]. 708:"Cooperation with Russia in aircraft engineering detailed" 516:"Balabuyev on importance of civilian aircraft production" 785:(in Russian). Vol. 5, no. 17. pp. 30–31. 151:
The An-180 was designed as a replacement for the aging
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The legend of Boeing. Part II: The lessons of Boeing.
806:"Defense industry, Russian-Ukrainian common interest" 1366: 1310: 1274: 1243: 1112: 1056: 808:. Defense Industry and Conversion: General Issues. 139:airliner. Although the design was completed by the 574: 321:, 10,305 kW (13,819 hp) each at take off 743:"Problems, situation in aviation industry viewed" 667:. November 21, 1994. pp. 23–24 – via 447:Brassey's World Aircraft & Systems Directory 251:Brassey's World Aircraft & Systems Directory 168:design with the propfan engines attached to the 989:: CS1 maint: others in cite AV media (notes) ( 778:[Promising engines of new generation]. 1033: 663:. Daily Report (published December 7, 1994). 573:Lenorovitz, Jeffrey M. (September 16, 1991). 8: 969:Salnikov, Yuri Petrovich (Director) (1991). 835:Karnozov, Vladimir (September 14–20, 2004). 290:4.3 m (14 ft 1 in) (fuselage) 450:. London, England, UK: Brassey's. pp.  1040: 1026: 1018: 895:"Antonov general designer on future plans" 714:. Daily Report (published March 1, 1995). 632:. International Affairs: Central Eurasia. 598:"Мечтать не вредно часть 2. Проект АН-180" 33:A design drawing of the proposed airliner 346:800 km/h (500 mph, 430 kn) 164:. As of September 1991, the An-180 had a 775:Перспективные двигатели нового поколения 439: 437: 435: 433: 431: 429: 425: 982: 972:Легенда Боинга. Фильм II. Уроки Боинга 893:Krikunenko, Anatoliy (November 1991). 689: 678: 15: 1005:from the original on October 19, 2007 903:Foreign Broadcast Information Service 814:Foreign Broadcast Information Service 751:Foreign Broadcast Information Service 728:Foreign Broadcast Information Service 718:. February 27, 1995. pp. 45–46. 669:Foreign Broadcast Information Service 638:Foreign Broadcast Information Service 524:Foreign Broadcast Information Service 493:Foreign Broadcast Information Service 483:Severyn, Volodymyr (March 27, 1993). 358:10,100 m (33,100 ft) cruise 7: 999:"An-180 project by ANTK O.K.Antonov" 582:Aviation Week & Space Technology 296:11.148 m (36 ft 7 in) 284:35.83 m (117 ft 7 in) 331:SV-27 axial contra-rotating tractor 278:40.9 m (134 ft 2 in) 741:Prudka, Natalka (August 3, 1995). 610:from the original on June 21, 2017 514:Stukalina, L. (October 13, 1990). 14: 1405:Abandoned civil aircraft projects 938:Aviatsiia I Kosmonavtika -Moskva- 899:Central Eurasia: Military affairs 810:Central Eurasia: Military affairs 804:Chernyak, I. (January 19, 1993). 518:. Defense Industrial Conversion. 485:"An-218 passenger plane profiled" 143:in 1994, the type was not built. 369: 302:42,500 kg (93,696 lb) 24: 1244:Reconnaissance and surveillance 772:Boguslaev, Vyacheslav (1999). 749:. Daily Report. Translated by 520:Soviet Union: Military affairs 444:Taylor, Michael J. H. (1996). 1: 1415:Twin-engined tractor aircraft 901:. JPRS Report. Translated by 812:. JPRS Report. Translated by 522:. JPRS Report. Translated by 491:. FBIS Report. Translated by 487:. Ukraine: Economic Affairs. 189:Production Corporation Polyot 87:Production Corporation Polyot 745:. Ukraine: Economic issues. 710:. Ukraine: Economic issues. 489:FBIS report: Central Eurasia 596:MakSiemens (May 13, 2013). 1431: 630:"Comments on carrier sale" 945:Aviation and astronautics 32: 23: 18: 1400:Propfan-powered aircraft 940: 932: 782: 774: 546:"Airliners of the world" 400:McDonnell Douglas MD-94X 646:2027/mdp.39015023043949 501:2027/inu.30000028466989 257:General characteristics 199:engines created by the 941:Авиация и космонавтика 661:Central Eurasia: Annex 316:Ivchenko Progress D-27 228:Ivchenko Progress D-27 201:Progress Design Bureau 91:Kharkiv Aviation Plant 874:]. Translated by 839:. Ukraine Aerospace. 327:8 fore, 6 aft-bladed 174:horizontal stabilizer 141:Antonov Design Bureau 77:Antonov Design Bureau 897:. Defense Industry. 842:Flight International 759:2027/nnc1.cu00734101 724:2027/nnc1.cu00733822 551:Flight International 306:Max takeoff weight: 1410:Low-wing aircraft 1382: 1381: 688:Missing or empty 585:. pp. 44–45. 579:. Air Transport. 237:unit load devices 121: 120: 1422: 1395:Antonov aircraft 1042: 1035: 1028: 1019: 1014: 1012: 1010: 994: 988: 980: 957: 956: 928: 915: 914: 890: 884: 883: 861: 855: 854: 832: 826: 825: 801: 795: 794: 769: 763: 762: 738: 732: 731: 704: 698: 697: 691: 686: 684: 676: 656: 650: 649: 636:. 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Index


Wide-body
propfan
airliner
Soviet Union
Ukraine
Antonov Design Bureau
Production Corporation Polyot
Kharkiv Aviation Plant
uk
Ukrainian
twin-aisle
propfan
Antonov Design Bureau
Tupolev Tu-134
Yakovlev Yak-42
Paris Air Show
T-tail
aft
horizontal stabilizer
wind tunnel
Kharkiv, Ukraine
Production Corporation Polyot
Omsk, Russia
D-27
Progress Design Bureau
CEO
Motor Sich
fuselage
Ivchenko Progress D-27

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