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Fundamentos de Aeronáutica I Aula 05 Modelos de Aeronaves - Construtores 2012 Prof. Dr. Odenir de Almeida Laboratório de Mecânica dos Fluidos UFU – Universidade Federal de Uberlandia Conteúdo 1. Evolução Histórica; 2. Principais Construtores; 3. Modelos Célebres de Aeronaves; 4. Apresentação de Aeronaves Civis em Atividade; 5. Apresentação de Aeronaves Militares em Atividade; Evolução Histórica Aviação Civil - Primeiras Companhias Aéreas • O uso de aeronaves para transporte de civis começou com o emprego de dirigíveis; • As primeiras tentativas remontam ao século XIX; http://en.wikipedia.org/wiki/File:Porter_02.jpg • A primeira companhia aérea foi a Deutsche Luftschiffahrts-Aktiengesellschaft DELAG, fundada em 16 de Novembro de 1909; • A DELAG operava dirigíveis construídos pela Zeppelin Corporation. Evolução Histórica Aviação Civil - Primeiras Companhias Aéreas • As primeiras companhias aéreas formadas e que ainda hoje operam vôos comerciais são: • KLM Avianca Qantas Czech • A KLM foi fundada em 7 de Outubro de 1919 e é considerada a companhia aérea mais antiga em operação; • Primeiro vôo da KLM em 17 de Maio de 1920 – Londres a Amsterdam • 1921 – Primeiro vôo para Bruxelas – Be. http://www.tca.viscal.net/klm/history/histo-1919-1928.htm Evolução Histórica Aviação Civil - Primeiras Companhias Aéreas • KLM http://www.tca.viscal.net/klm/history/histo-1919-1928.htm Evolução Histórica Aviação Militar - Primeiras Aeronaves • No contexto histórico, a primeira aeronave militar foi o Wright Flyer, formalmente aceito em 02 de Agosto de 1909 pela US Army Signal Corps; • Durante a I Guerra Mundial, as aeronaves eram utilizadas principalmente como aviões de reconhecimento; http://en.wikipedia.org/wiki/File:Wright_Military_Flyer_arrives_at_Fort_Myer_VA_DA-SD-05-00659.JPEG The Wright 1908 Model A Military Flyer arrives at Fort Myer, Virginia aboard a wagon, attracting the attention of children and adults Principais Construtores Aviação Civil • Ao longo do século XX vários construtores de aeronaves se estabeleceram. Muitos ainda estão em atividades até os dias atuais, outros não sobreviveram as mudanças de mercado e competição técnica e empresarial. Pode-se citar algumas empresas como: McDonnell Douglas (US) Fokker (Holanda) BAE (UK) Airbus (França) ATR (França/Itália) Boeing (US) Dassault (França) Embraer (Brazil) CESSNA (US) Bombardier (Canadá) Dornier (Alemanha) SAAB (Suécia) Mitsubishi (Japão) Beechcraft (US) Gulfstream (US) outras… • Existem muitas outras empresas de aviação de pequeno e médio porte ao redor do mundo produzindo aeronaves certificadas ou experimentais. Um exemplo no Brasil é a Aeroalcool S.A. Principais Construtores Aviação Militar • De acordo com a história da aviação o avião foi primeiramente empregado na área militar, como o caso do Wright Flyer (1909) e todas as demais aeronaves que operaram na I Guerra Mundial; • Dentro deste contexto muitas empresas surgiram e desapareceram ao longo do século XX, muitas unindo projetos militares e civis e outras apenas focando no projeto e construção de aeronaves militares. Podem-se citar: Fokker (Holanda) Airbus (França) Boeing (US) Dassault (França) Embraer (Brazil) SAAB (Suécia) Mitsubishi (Japão) entre outras… Modelos Célebres de Aeronaves Aviação Civil • Na sequencia são apresentados modelos considerados célebres de aeronaves, tendo em vista características peculiares do projeto e operação, tais como novos conceitos, tecnologias, tempo em serviço, característica de operação etc; • É importante que se tenha o conhecimento das principais características dessas aeronaves. Uma ficha técnica resumida é também fornecida. Modelos Célebres de Aeronaves Aviação Civil Douglas DC-3 First Flight: December 17, 1935 Number Built: 10,654 produced from 1935 thru 1949 Length: 64 feet 6 inches Wing Span: 95 feet Height: 16 feet 11 inches Max Take-Off Wt.: 28,000 lbs. Max Landing Wt.: N/A Empty Wt.: 16,970 lbs. Max Cruising Speed: 229 mph 198 kts @ 7500 feet Normal Cruising Speed: 182 mph 157 kts Approach Speed: 103 mph 90 kts Landing Speed: 92 mph 80 kts Stall Speed: 66 mph 58 kts Service Ceiling: 23,200 feet Fuel Capacity: 804 US gallons Range: 1500 miles Fuel Type: 100/130 octane Fuel Consumption: 100 gph both flight plan burn Engines: 2 Pratt & Whitney R-1830 or 2 Wright Cyclone R-1820 Seating: 21 Passengers Crew: 2 Pilots and 1 Flight Attendant Engine Specifications Pratt & Whitney R-1830 Type: 14 cylinder air cooled radial Length: 52 inches Bore: 5.50 inches Stroke: 5.50 inches Displacement: 1830 cubic inches Compression Ratio: 6.7 to 1 Dry Weight: 1162 to 1467 lbs Ignition: Dual Scintilla Fuel Grade: 100/130 octane Carburation: Stromberg Performance: 1250 HP @ 2700 rpm Modelos Célebres de Aeronaves Aviação Civil Douglas DC-3 Modelos Célebres de Aeronaves Aviação Civil Ford Trimotor Crew 2 Passengers 17 Propulsion 3 Radial Engines Engine Model Pratt & Whitney C-1 Wasp Engine Power (each) 313 kW 420 hp max. Cruise Speed 196 km/h 106 kts 122 mph max. Speed (vne) 241 km/h 130 kts 150 mph Service Ceiling 5.639 m 18.500 ft Range 885 km 478 NM 550 mi. Empty Weight 3.556 kg 7.840 lbs max. Takeoff Weight 6.123 kg 13.499 lbs Wing Span 23,72 m 77,8 ft Wing Area 77,6 m² 835 ft² Length 15,32 m 50,3 ft Height 3,86 m 12,7 ft First Flight 11. Feb. 1926 Production Status out of production Total Production 199 Developed from Stout 2-AT Pullman ICAO Code TRIM Data for (Version) Ford 5-AT-D Tri Motor Variants Ford 4-AT-A, 4-AT-B, 4-AT-D, 4-AT-E, 5-AT-A, 5-AT-B, 5-AT-C, 5-AT-D, 6-AT-A, C-3A (C-9A), C-4A, JR-2 (RR-2), JR-3 (RR-3) Modelos Célebres de Aeronaves Aviação Civil Ford Trimotor Modelos Célebres de Aeronaves Aviação Civil Sikorsky S-42 Flying Boat - Clipper Development: Manufactured by the Vought-Sikorsky Aircraft Division of the United Aircraft Corporation in Stratford, Connecticut.. The aircraft first flew on March 30, 1934. A total of 10 aircraft were built. These were the first of the great Pan American Airways Clipper Flying Boats and the first true over ocean transport. Modifications: Model S42A upgraded engines, an improved airfoil, an increased wingspan, a stronger and lighter aluminum alloy skin, a larger gross weight and useful load and convertible sleeping accommodations for 14 passengers; Four aircraft built to this configuration. The Model S42B made additional aerodynamic improvements, increase in gross weight, improved fuel capacity and thus distance, and the addition of constant speed propellers enhanced the performance; Three were built to this configuration. Service: With Pan American Airways. Crew: 4 Wingspan: 118 feet 2 inches / 36 m Length: 69 feet / 21 m Height: 21 feet 9 inches / 6.7 m Gross Weight: 42000 lbs Engines: 4x Pratt & Whitney Hornet Radial Engines (750 horsepower each) Maximum Speed: 190 mph Cruise Speed: 150 mph / Cruise Ceiling: 16000 feet Range: 1200 miles Payload: 28-32 passengers Modelos Célebres de Aeronaves Aviação Civil Sikorsky S-42 Flying Boat - Clipper Modelos Célebres de Aeronaves Aviação Civil Lockheed Constellation Lockheed Constellation Specifications: Dimensions: Model 1649 Wing span: 150 ft 0 in (45.72 m) Length: 116 ft 2 in (35.41 m) Height: 24 ft 9 in (7.54 m) Wing Area: 1,850 ft² (171.87 m²) Weights: Empty Weight: 91,645 lbs (41,969 kg) Loaded Weight: 160,000 lbs (72,575 kg) Performance: Max. Speed: 377 mph (606 km/h) @ 18,600 ft (5,669 m) Cruising Speed: 290 mph (466 km/h) Service Ceiling: 23,700 ft (7,223 m) Max Range: 6,180 miles (9,945 km) with 8,000 lb (3,628 kg) payload Range Max Payload: 4,940 miles (7,950 km) with 19,500 lb (8,845 kg) payload Powerplant: Four Wright Cyclone R-3350-988TC-18EA-2 turbo-compound rated @ 3,400 hp (2,535 kw) each Modelos Célebres de Aeronaves Aviação Civil Lockheed Constellation Modelos Célebres de Aeronaves Aviação Civil Boeing 377 Stratocruiser Specifications First flight: July 8, 1947 Model number: 377 Classification: Commercial transport Span: 141 feet 3 inches Length: 110 feet 4 inches Gross weight: 145,000 pounds Top speed: 375 mph Cruising speed: 300 mph Range: 4,600 miles Ceiling: More than 33,000 feet Power: Four 3,500-horsepower P&W R-4360 Wasp Major engines Accommodation: 55 to 100 passengers and attendants Specifications Modelos Célebres de Aeronaves Aviação Civil Boeing 377 Stratocruiser Modelos Célebres de Aeronaves Aviação Civil De Havilland D.H.106 Comet Crew 4 Passengers 78, max. 99 (Comet 4) Propulsion 4 Turbojet Engines Engine Model Rolls-Royce Avon 524 Engine Power (each) 51,2 kN 11500 lbf Speed 900 km/h 486 kts 559 mph Service Ceiling 12.192 m 40.000 ft Range 5.186 km 2.800 NM 3.222 mi. Empty Weight 34.212 kg 75.425 lbs max. Takeoff Weight 73.482 kg 162.000 lbs Wing Span 35,00 m 114,8 ft Wing Area 197,0 m² 2120 ft² Length 33,99 m 111,5 ft Height 8,99 m 29,5 ft First Flight 27.07.1949 Production Status out of production Total Production 125 Data for (Version) de Havilland Comet 4 Variants Comet 1, Comet 1A, Comet 1XB, Comet T2, Comet C2, Comet 2R, Comet 3, Comet 4B, Comet 4C, Comet C.4 The de Havilland D.H.106 Comet is a four-engine medium- to longe-range airliner with a capacity of max. 99 passengers produced by the British manufacturer de Havilland Aircraft Company. Modelos Célebres de Aeronaves Aviação Civil De Havilland D.H.106 Comet Modelos Célebres de Aeronaves Aviação Civil Lockheed L-188 Electra The Lockheed L-188 Electra is a four-engine short- to medium-range turboprop airliner for up to 99 passengers produced by the US-American manufacturer Lockheed Corporation. Many Electra had been converted as cargo freighters after their service as airliners. Crew 3 Passengers 99 Propulsion 4 Turboprop Engines Engine Model Allison 501D-13 Engine Power (each) 2796 kW 3750 shp max. Cruise Speed 600 km/h 324 kts 373 mph max. Speed (vne) 674 km/h 364 kts 419 mph Service Ceiling 9.144 m 30.000 ft Range 3.541 km 1.912 NM 2.200 mi. Empty Weight 26.036 kg 57.400 lbs max. Takeoff Weight 51.256 kg 113.000 lbs Wing Span 30,18 m 99,0 ft Wing Area 120,8 m² 1300 ft² Length 31,85 m 104,5 ft Height 10,01 m 32,8 ft First Flight 06.12.1957 Production Status out of production Production Range 1958-1961 Total Production 170 FAA TCDS 4A22 Data for (Version) Lockheed L-188A Electra Variants L-118A, L-188C Modelos Célebres de Aeronaves Aviação Civil Lockheed L-188 Electra Modelos Célebres de Aeronaves Aviação Civil Boeing 707 The Boeing 707 is a four-engined medium-to-long-range narrowbody airliner with a capacity of maximum 189 passengers produced by the American manufacturer Boeing Commercial Airplanes. Advanced 707-320B Wingspan 145 feet 9 inches (44.42 m) Length 152 feet 11 inches (46.6 m) Wing Area 3,010 square feet (280 m2) Gross Weight 336,000 pounds (152,400 kg) Cruising Speed 607 mph (977 km/h) Range 6,160 miles (9,913 km) Service Ceiling 36,000 feet (10,973 m) Power Four Pratt & Whitney JT3D turbofans of 18,000 pounds thrust each Passenger Cabin 141 passengers mixed class or a maximum of 189 all economy Specifications Modelos Célebres de Aeronaves Aviação Civil Boeing 707 Modelos Célebres de Aeronaves Aviação Civil Douglas DC-8 The Douglas DC-8 is a four-engine long-range Jet Airliner with a capacity of maximum 259 passengers produced by the US-American manufacturer Douglas Aircraft Company. Specifications Crew 3 Passengers 259 Propulsion 4 Turbofan Engines Engine Model Pratt & Whitney JT3D-7 Engine Power (each) 84,5 kN 19000 lbf Speed 967 km/h 522 kts 601 mph Service Ceiling 12.802 m 42.000 ft Range 3.445 km 1.860 NM 2.140 mi. Empty Weight 69.740 kg 153.750 lbs max. Takeoff Weight 158.750 kg 349.984 lbs Wing Span 45,24 m 148,4 ft Wing Area 271,9 m² 2927 ft² Length 57,12 m 187,4 ft Height 12,93 m 42,4 ft First Flight 30.05.1958 Production Status out of production Total Production 556 ICAO Code DC85 / DC86 / DC87 Data for (Version) Douglas DC-8-63 Modelos Célebres de Aeronaves Aviação Civil Douglas DC-8 Apresentação de Aeronaves Civis em Atividade Principais aeronaves civis em atividade: • Na sequencia serão apresentadas algumas aeronaves civis em atividade: Apresentação de Aeronaves Civis em Atividade Boeing 737 Family: 737-900ER Passengers Typical 2-class configuration 180 Typical 1-class configuration 215 Cargo 1,827 cu ft (51.7 cu m) 1,673 cu ft (47.3 cu m) w/aux. tank 1,585 cu ft (44.9 cu m) w/2 aux. tanks Engines (maximum thrust) CFMI CFM56-7 27,300 lb Maximum Fuel Capacity 7,837 U.S. gal (29,660 L) (2 aux tanks) Maximum Takeoff Weight 187,700 lb (85,130 kg) Maximum Range 3,265 nautical miles (6,045 km) [2-class with winglets and 2 aux fuel tanks] Typical Cruise Speed (at 35,000 feet) 0.78 Mach Basic Dimensions Wing Span With Winglets 112 ft 7 in (34.3 m) 117 ft 5 in (35.7 m) Overall Length 138 ft 2 in (42.1 m) Tail Height 41 ft 2 in (12.5 m) Interior Cabin Width 11 ft 7 in (3.53 m) 737-900ER 737-200 Apresentação de Aeronaves Civis em Atividade Boeing 747 Family: 747-900ER 747-100 747-400ER Passengers Typical 3-class configuration Typical 2-class configuration 416 524 Cargo* 5,599 cu ft (158.6 cu m) or 4,837 cu ft (137 cu m) Engines maximum thrust Pratt & Whitney PW4062 63,300 lb (281.57 kN) General Electric CF6-80C2B5F 62,100 lb (276.23 kN) Maximum Fuel Capacity** 63,705 U.S. gal (241,140 L) Maximum Takeoff Weight 910,000 lb (412,770 kg) Maximum Range 7,670 nautical miles (14,205 km) Typical city pairs: New York - Hong Kong Los Angeles - Melbourne Rio - Perth Typical Cruise Speed at 35,000 feet 0.855 Mach 567 mph (913 km/h) Basic Dimensions Wing Span Overall Length Tail Height Interior Cabin Width 211 ft 5 in (64.4 m) 231 ft 10 in (70.6 m) 63 ft 8 in (19.4 m) 20 ft (6.1 m) Apresentação de Aeronaves Civis em Atividade Boeing 767 Family: Boeing 767-400ER Passenger Seating Configuration Typical 3-class Typical 2-class Typical 1-class 245 304 375 Cargo 5,095 cu ft (144.3 cu m) Engines maximum thrust Pratt & Whitney PW4000 63,300 pounds General Electric CF6-80C 63,500 pounds Maximum Fuel Capacity 23,980 U.S. gal (90,770 L) Maximum Takeoff Weight 450,000 pounds (204,120 kg) Maximum Range 5,625 nautical miles (10,415 km) Typical city pairs: London to Tokyo, Newark to Moscow Chicago to Warsaw Typical Cruise Speed at 35,000 feet Mach 0.80 (530 mph, 851 kph) Basic Dimensions Wing Span Overall Length Tail Height Interior Cabin Width 170 ft 4 in (51.9 m) 201 ft 4 in (61.3 m) 55 ft 4 in (16.8 m) 15 ft 6 in (4.7 m) Apresentação de Aeronaves Civis em Atividade Boeing 777 Family: Crew 2 Passengers max. 550 Propulsion 2 Turbofan Engines Engine Model Rolls-Royce Trent 892 Engine Power (each) 400 kN 90000 lbf Speed 950 km/h 513 kts 590 mph Mmo (max. Mach) Mach 0.84 Service Ceiling 13.137 m 43.100 ft Range 11.140 km 6.015 NM 6.922 mi. Empty Weight 159.570 kg 351.700 lbs max. Takeoff Weight 299.370 kg 660.000 lbs max. Landing Weight 237.680 kg 524.000 lbs Wing Span 60,93 m 199,9 ft Wing Area 427,8 m² 4605 ft² Length 73,80 m 242,1 ft Height 18,51 m 60,7 ft First Flight 16.10.1997 Production Status in production Developed from 777-200 ICAO Code B773, B77W FAA TCDS T00001SE EASA TCDS A.003 Data for (Version) Boeing 777-300 Variants 777-300, 777-300ER Apresentação de Aeronaves Civis em Atividade Airbus A-320 Family: A-320 A-318 Crew 2 Passengers 150 / 179 Propulsion 2 Turbofan Engines Engine Model IAE International Aero Engines V2527-A5 Engine Power (each) 110,3 kN 24800 lbf Speed 904 km/h 488 kts 562 mph Mmo (max. Mach) Mach 0.82 Service Ceiling 12.131 m 39.800 ft Range 5.700 km 3.078 NM 3.542 mi. Empty Weight 37.230 kg 82.078 lbs max. Takeoff Weight 77.000 kg 169.756 lbs max. Landing Weight 64.500 kg 142.198 lbs Wing Span 34,09 m 111,8 ft Wing Area 122,6 m² 1320 ft² Length 37,57 m 123,3 ft Height 11,76 m 38,6 ft First Flight 22.02.1987 Production Status in production ICAO Code A320 IATA Code 320 FAA TCDS A28NM EASA TCDS A.064 Data for (Version) Airbus A320-232 Variants A320-111, A320-211, A320-212, A320-214, A320- 215, A320-216, A320-231, A320-232, A320-233 Apresentação de Aeronaves Civis em Atividade Airbus A340-500 Crew 2 Passengers typ. 380, max. 440 Propulsion 4 Turbofan Engines Engine Model Rolls-Royce Trent 556-61 Engine Power (each) 260,1 kN 58462 lbf Speed 915 km/h 494 kts 568 mph Mmo (max. Mach) Mach 0.86 Service Ceiling 12.634 m 41.450 ft Range 14.599 km 7.883 NM 9.072 mi. Empty Weight 240.000 kg 529.109 lbs max. Takeoff Weight 368.000 kg 811.300 lbs max. Landing Weight 259.000 kg 570.997 lbs Wing Span 63,45 m 208,2 ft Wing Area 439,4 m² 4730 ft² Length 75,30 m 247,0 ft Height 17,30 m 56,8 ft First Flight 23.04.2001 Production Status in production Developed from Airbus A340-300 ICAO Code A346 IATA Code 346 FAA TCDS A43NM EASA TCDS A.015 Data for (Version) Airbus A340-642 Variants A340-642, A340-643 Apresentação de Aeronaves Militares em Atividade Principais aeronaves militares em atividade: • Na sequência serão apresentadas algumas aeronaves militares em atividade: AMX F-117 Nighthawk F5 F-22 Raptor Hércules C-130 B-52 F-16C Fighting Falcon MiG-29 Fulcrum A-10 Thunderbolt Apresentação de Aeronaves Militares em Atividade AMX A-1 (Aeritalia-Aermacchi-Embraer): Crew 1 Propulsion 1 Turbofan Engine Engine Model Rolls-Royce RB.168 Spey Mk.807 Engine Power 49,1 kN 11038 lbf Speed 915 km/h 494 kts 568 mph Service Ceiling 13.000 m 42.651 ft Range 3.330 km 1.798 NM 2.069 mi. Empty Weight 6.700 kg 14.771 lbs max. Takeoff Weight 12.500 kg 27.558 lbs Wing Span 8,87 m 29,1 ft Wing Area 21,0 m² 226 ft² Length 13,23 m 43,4 ft Height 4,55 m 14,9 ft First Flight 15.05.1984 Production Status out of production Production Range 1986-1999 ICAO Code AMX Data for (Version) AMX International AMX Apresentação de Aeronaves Militares em Atividade F-5 Freedom Fighter (Northrop): Crew 1 Propulsion 2 Turbojet Engines Engine Model General Electric J85-GE-21 Engine Power (each) 22,2 kN 5000 lbf Speed 1743 km/h 941 kts 1083 mph Service Ceiling 15.789 m 51.800 ft Range 1.406 km 759 NM 873 mi. Empty Weight 4.410 kg 9.722 lbs max. Takeoff Weight 11.214 kg 24.723 lbs Wing Span 8,13 m 26,7 ft Wing Area 17,3 m² 186 ft² Length 14,45 m 47,4 ft Height 4,06 m 13,3 ft First Flight 30.07.1959 Production Status out of production Total Production 2622 Data for (Version) Northrop F-5E Tiger II Variants A-9 (F-5A), AR-9, CF-5 (CF-116), F-5A, F-5B, F- 5E Tiger II, F-5E Tiger III, F-5EM, F-5F Tiger II, F- 5F Tiger III, F-5FM, F-5N, F-5S, F-5T, F-5T Tigris, F-5TIII, KF-5E, KF-5F, NF-5A Apresentação de Aeronaves Militares em Atividade C-130 Hércules (Lockheed): Crew 3 (2) Propulsion 4 Turboprop Engines Engine Model Allison (Rolls-Royce) T56-A-15 (AE 2100D3) Engine Power (each) 3362 (3460) kW 4509 (4640) shp Speed 650 (670) km/h 351 (362) kts 404 (417) mph Mmo (max. Mach) Mach 0.77 Service Ceiling 10.058 (8.534) m 33.000 (28.000) ft Range 4.002 (5.250) km 2.161 (2.835) NM 2.487 (3.262) mi. Empty Weight 37.648 (34.274) kg 83.000 (75.562) lbs max. Takeoff Weight 70.307 (79.379) kg 155.000 (175.000) lbs Wing Span 40,41 m 132,6 ft Wing Area 162,1 m² 1745 ft² Length 29,79 m 97,7 ft Height 11,61 m 38,1 ft First Flight 23.08.1954 Production Status in production ICAO Code C130, C30J Data for (Version) Lockheed C-130H (C-130J) Hercules Variants L-100, L-100-20, L-100-30, C-130A, C-130B, C- 130D, C-130E, C-130F, C-130G, C-130H, C-130J, C-130K (Hercules C.4/C.5), C-130T, EC-130, HC- 130, KC-130, LC-130, MC-130, PC-130, RC-130 Apresentação de Aeronaves Militares em Atividade F-16C Fighting Falcon (General Dynamics / Lockheed): Crew 1 Propulsion 1 Turbofan Engine Engine Model General Electric F110-GE-129 Engine Power 129,1 kN 29023 lbf Speed 2200 km/h 1188 kts 1367 mph Service Ceiling 18.288 m 60.000 ft Range 1.600 km 864 NM 994 mi. Empty Weight 8.437 kg 18.600 lbs max. Takeoff Weight 19.187 kg 42.300 lbs Wing Span 10,00 m 32,8 ft Wing Area 27,9 m² 300 ft² Length 15,02 m 49,3 ft Height 5,09 m 16,7 ft First Flight 20. Jan 1974 Production Status in production Data for (Version) General Dynamics F-16C Block 50 Variants F-16A/B, F-16C/D, F-16E/F Apresentação de Aeronaves Militares em Atividade A-10 Thunderbolt (Fairchild US): Crew 1 Propulsion 2 Turbofan Engines Engine Model General Electric TF34-GE-100 Engine Power (each) 40,4 kN 9071 lbf Speed 706 km/h 381 kts 438 mph Service Ceiling 13.716 m 45.000 ft Range 1.287 km 695 NM 800 mi. Empty Weight 12.700 kg 28.000 lbs max. Takeoff Weight 23.586 kg 52.000 lbs Wing Span 17,53 m 57,5 ft Wing Area 47,0 m² 506 ft² Length 16,26 m 53,3 ft Height 4,47 m 14,7 ft First Flight 10.05.1972 Production Status out of production Total Production 713 Data for (Version) Republic A-10A Thunderbolt II Variants A-10A, OA-10A Apresentação de Aeronaves Militares em Atividade F-117 Nighthawk (Lockheed): Crew 1 Propulsion 2 Turbofan Engines Engine Model General Electric F404-GE-F1D2 Engine Power (each) 48 kN 10809 lbf Speed 1041 km/h 562 kts 647 mph Service Ceiling 21.031 m 69.000 ft Range 1.721 km 929 NM 1.069 mi. Empty Weight 13.609 kg 30.003 lbs max. Takeoff Weight 23.814 kg 52.501 lbs Wing Span 13,20 m 43,3 ft Wing Area 73,0 m² 786 ft² Length 20,09 m 65,9 ft Height 3,78 m 12,4 ft First Flight 18.06.1981 Production Status out of production Production Range 1981-1990 Total Production 64 Data for (Version) Lockheed F-117A Nighthawk Apresentação de Aeronaves Militares em Atividade F-22 Raptor (Lockheed): Crew 1 Propulsion 2 Turbofan Engines Engine Model Pratt & Whitney F119-PW-100 Engine Power (each) dry/with Afterburner 116 / 156 kN 26000 / 35000 lbf Speed 1915 km/h 1034 kts 1190 mph Mmo (max. Mach) Mach 2.0 Service Ceiling 19.812 m 65.000 ft Range 2.963 km 1.600 NM 1.841 mi. Empty Weight 19.659 kg 43.340 lbs max. Takeoff Weight 37.875 kg 83.500 lbs Wing Span 13,56 m 44,5 ft Wing Area 78,0 m² 840 ft² Length 18,90 m 62,0 ft Height 5,09 m 16,7 ft First Flight 07.09.1997 Production Status in production Data for (Version) Lockheed F-22 Raptor Apresentação de Aeronaves Militares em Atividade B-52 Stratofortress (Boeing): Crew 5 Propulsion 8 Turbofan Engines Engine Model Pratt & Whitney TF33-P-3 Engine Power (each) 75,6 kN 17000 lbf Speed 957 km/h 517 kts 595 mph Service Ceiling 15.240 m 50.000 ft Range 14.172 km 7.652 NM 8.806 mi. Empty Weight 111.350 kg 245.485 lbs max. Takeoff Weight 251.353 kg 554.139 lbs Wing Span 56,39 m 185,0 ft Wing Area 371,6 m² 4000 ft² Length 49,05 m 160,9 ft Height 12,40 m 40,7 ft First Flight 15.04.1952 Production Status out of production Production Range 1952-1962 Total Production 744 ICAO Code B52 Data for (Version) Boeing B-52H Stratofortress Apresentação de Aeronaves Militares em Atividade MiG-29 Fulcrum (Mikoyan-Gurevich): Crew 1 Propulsion 2 Turbofan Engines Engine Model Klimow / Klimov RD-33 Engine Power (each) dry/with Afterburner 49,6 / 81 kN 11151 / 18210 lbf Speed 2465 km/h 1331 kts 1532 mph Service Ceiling 18.500 m 60.695 ft Range 1.500 km 810 NM 932 mi. Empty Weight 11.200 kg 24.692 lbs max. Takeoff Weight 19.700 kg 43.431 lbs Wing Span 11,36 m 37,3 ft Wing Area 38,0 m² 409 ft² Length 17,32 m 56,8 ft Height 4,73 m 15,5 ft First Flight 06.10.1977 Production Status in production NATO Code Fulcrum Data for (Version) Mikoyan-Gurevich / Mikojan-Gurewitsch MiG-29S, SE