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Sukhoi Su-5

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near the end of World War II prompted the Soviet Union to develop faster fighter aircraft. Since the USSR lacked a production-ready turbojet engine, development efforts were directed toward mixed-power aircraft utilizing a conventional piston engine-driven propeller for the majority of propulsion
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A piston engine was damaged beyond repair in flight. Following acquisition of another VK-107A, flight testing continued until 18 October when the engine reached the end of its service life. No further VK-107As could be procured and the project was canceled.
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wing and attained 793 km/h (428 kn, 493 mph) at 4,350 m (14,270 ft) with the motorjet functioning. On 15 June 1945, the
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were designed in 1944. The aircraft first flew on 6 April 1945 and underwent limited flight testing. It was subsequently fitted with a
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Antonov, Vladimir; Gordon, Yefim; Gordyukov, Nikolai; Yakovlev, Vladimir; Zenkin, Vyacheslav; Carruth, Lenox; Miller, Jay (1996).
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V-12 liquid-cooled piston engine, 1,230 kW (1,650 hp) at 8,300 m (27,200 ft)
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Istoriia konstruktskii samoletov v SSSR, 1938–1950, The Great Book of Fighters, OKB Sukhoi
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810 km/h (500 mph; 440 kn) at 7,800 m (25,600 ft)
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793 km/h (493 mph, 428 kn) at 4,350 m (14,270 ft)
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OKB Sukhoi : a history of the design bureau and its aircraft
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Istoriia konstruktskii samoletov v SSSR, 1938–1950 gg. (3 izd.)
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booster, 2.9 kN (650 lbf) thrust for 10 minutes (
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Abandoned military aircraft projects of the Soviet Union
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The Su-5 (initially I-107) and the conceptually similar
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with a small rocket or jet engine for bursts of speed.
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5,000 m (16,000 ft) in 5 minutes 42 seconds
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Aircraft of comparable role, configuration, and era
986: 550: 404: 263:Воздушно-Реактивный Двигатель Компрессорный 160:Воздушно-Реактивный Двигатель Компрессорный 557: 543: 267:Vozdushno-Reaktivny Dvigatel Kompressornyi 400: 398: 396: 165: 514:"The Incomplete Guide to Airfoil Usage" 428: 426: 315:600 km (370 mi, 320 nmi) 987: 480: 393: 538: 451: 154:of all-metal construction. The VRDK ( 511: 505: 423: 564: 201:10.56 m (34 ft 8 in) 195:8.51 m (27 ft 11 in) 13: 14: 1031: 433:Green, W; Swanborough, G (2001). 275:4-bladed constant-speed propeller 207:17 m (180 sq ft) 321:12,050 m (39,530 ft) 269:– air reaction compressor jet) 117: 1: 1005:1940s Soviet fighter aircraft 386: 237:3,804 kg (8,386 lb) 231:2,954 kg (6,512 lb) 122:The appearance of the German 1020:Aircraft first flown in 1945 150:The Su-5 was a conventional 7: 367: 357:2 × 12.7 mm (0.50 in) 106:mixed-power (propeller and 10: 1036: 435:The Great Book of Fighters 219:TsAGI 1B10 (16.5%) ; 1000:Motorjet-powered aircraft 969: 928: 912: 801: 780: 759: 733: 717: 651: 573: 361:machine guns with 200 rpg 350:1 × 23 mm (0.91 in) 159: 84: 79: 71: 63: 51: 39: 31: 26: 21: 16:Soviet fighter prototype 974:List of Sukhoi aircraft 574:Fighters / interceptors 518:m-selig.ae.illinois.edu 180:General characteristics 379:Mikoyan-Gurevich I-250 354:cannon with 100 rounds 352:Nudelman-Suranov NS-23 136:Mikoyan-Gurevich I-250 734:Competitive aerobatic 463:Sukhoi Company Museum 405:Shavrov V.B. (1994). 166:Specifications (Su-5) 995:Mixed-power aircraft 128:Messerschmitt Me 262 409:. Mashinostroenie. 257:main-engine driven 27:General information 956:T-12 Shturmovik-90 929:Cancelled projects 437:. MBI Publishing. 982: 981: 512:Lednicer, David. 325:Time to altitude: 92: 91: 1027: 652:Bombers / attack 559: 552: 545: 536: 535: 529: 528: 526: 524: 509: 503: 502: 484: 478: 477: 475: 474: 465:. 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Index

Manufacturer
Sukhoi
Pavel Sukhoi
Soviet
motorjet
World War II
turbojet
Messerschmitt Me 262
Mikoyan-Gurevich I-250
laminar flow
Klimov VK-107
monoplane
Russian
Airfoil
NACA 23011
Klimov VK-107A
VRDK
thermojet
Nudelman-Suranov NS-23
Berezin UB
Mikoyan-Gurevich I-250



ISBN
5-217-00477-0


ISBN
0-7603-1194-3

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