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Aviation History
1995
1995 - 3151.PDF
MILITARY AIRCRAFT OF THE WORLD 4100 15.63 5315 0460 (ground roll @ 3.500kg)440 hi-lo-lo-hi (Mil-C-5011B-USAF)0 500042320(WTO 3,700kg) No2340km (a)/4h 20mln (a)30mm canon pod, 2 x MK82, 2 x MK81 (bombs) Mikoyan 10.16 12.01 17.67 Russia MiG-AT2 x Turbomeca/Snecma Larzac 04-R20 turbofans 14.12kN 4610 460kt850kg+200kg in wing 470 0 0 7000 0 0 570 tandem 0 50850 No 3000km (a)/ prototype (a) ferry range; contender for Russian air force trainer programme NAMC, PAC (Pakistan Aeronautical Complex) China. Pakistan K-8 Karakorum 81 x AlliedSignal TFE731-2A turbofan 16.01kN 9.63 2687 435kt 1700lit 424 943 0 11.6 3630 5315 388 500 0 tandem production (a) max int/ext fuel 17.02 4330 42650 No2202km (a)/4h 25min (a) 1 x 23mm (opt) Siai-Marchetti SRL Italy S.2111 x Pratt & Whitney Canada JT15D-4C turbofanll.lkN production 8.43 1960 360kt/0.8M 800lit(a) 615 750 5 9.5 2750 3550 530 360 550 hi-lo-lo tandem 12.6 3250 40000 No 1500km/3h(b)gun pods 7.62/12.7/20mm->330kg, rocket launcher ___^ up to 100mm (a) max int fuel 30min reserves; (b) 30min reserves; load factor +6G • 3G: sustained load factor si 3.3G Sukhoi 9.08 12.3 26.42 Russia Su-542 x Soyuz Tumansky R-195FS turbojets41.2kN dry/60.8kN reheatprototype 4790 890kt/155M 1660kg 380 0 0 9410 0 0 500 tandem 0 59050 No 2000km (a) (a) max internal fuel Russian air force requirement, first Yakovlev Design Bureau 10.64 11.3 0 6200 9000 Russia Yak-1301 x PSAS Slovakia/Klimov RD-35 turbofan21.56kN development 576kt/ 1800lit 380 0 0 14173 0 670-520 tandem 41010 No 2000km in competition with Mikoyan for flight at end 1995 Short Brothers UKTucano TMK501 x AlliedSignal Garrett TPE331-12B turboprop production 11.28 2232 255kt 695lit760 (to 50ft 3,600kg) 1030 4 9.86 3600 2390 640 790 (from 50ft 3.600kg)721 + 5min on station with 500kg 0 19.4 0 34000 No2104km/6hl2min • Aero Vodochody Czech Republic L-1391 x AlliedSignal TFE731-4-1T turbofan 18.16kN development 9.46 3460 410kt 1260lit 540 1500 4 12.13 6000 4400 1400 610 0 tandem 18.8 6000 38725 Nol600km (a)/3h 20min (b) 1 x 23mm Aero Vodochody Czech Republic L-591 x PS Povazska Bystrica DV-2 turbofan 21.6kN production 9.54 4030 470kt 1540lit 600 1500 4 12.2 7000 4921 1400 720 0 tandem 18.8 7000 38725 Noll60km (a)/2h 40min (b) 1 x 23mm (a) 2,900km with ext fuel tanks (4 x 350 litres); (b) 6h with ext fuel tanks (a) 2,500km with ext fuel tanks (4 x 350 litres); (b) 4h 50min with ext fuel tanks Aero Vodochody Czech RepublicL-39ZA Albatrosl x ZMKB Progress AI-25TL turbofan 16.9kN production 9.46 3400 405kt 1260lit 540 1500 4 12.13 5670 4130 1400 690 0 tandem 18.8 5670 34776 NollOOkm (a)/2h 30min (b) lx23mm (a) 2,500km with ext fuel tanks (4 x 350 litres): (b) 5h with ext fuel tanks Class Manufacturer Manf Colab Span Empty weight (kg) Length (m) Max TO Wing area (m2) MTOW armed ..;?l?h:t»i?j.'BriEr- Country Type Max speedlnital climb (ft/min) Cruise speed Ceiling ft Stall speed Int fuel (litres) Powerplant Kw Status TO run m Endurance h/min No Hardpoints Landing run m Combat radius km Capacity pax Range km Warload kg Armament ran Aero Vodochody Czech Republic L-39C Albatros 1 x ZMKB Progress AI-25TL turbofan 9.46 3455 405kt 4330 530 12.13 4800 36090 65 18.8 90 1260 1100 (a) 16.9kN 2h 30min (a) 250 production 2 tandem Additional info/remarks stall speed is kt landing configuration; (a) 23,000ft, internal fuel British Aerospace Defence UK 9.4 4012 545kt/0.82M 12.4 9100 16.7 90 Hawk 601 x Rolls-Royce Turbomeca Adour 861 turbofan 25.4kN production 11800 550 4h 5 46000 520 741 hi-lo-lo-hi tandem 1655 2918(a) 3000 1 x 30mm,2xAAM (a) ferry with 2 x 590 litre tanks HAL 10.7 10.6 19 India 2995 382W/0.58M 4250 206kt/0.35M 5000 89 Kiran Mk.lll x Rolls-Royce Orpheus 70105 turbojet 4626 540 30000 93 1340 780 (a) 18.68kN production side-by-side (a) 29,000ft or 510km at 9,840ft Kawasaki Heavy Industries Japan T-4 9.9 3700 560kt/0.91M 10000 13 5500 0.75M 50000 21 7500 90 2240 2 x IHI F3-IHI-30 turbofans 550 (a) 670 (a) 1300 (a & b) 32.7kN production 3 tandem initial climb and (a) is at 5,500kg, (b) internal fuel only McDonnell DouglasBritish Aerospace USA, UK 9.4 4638 534kt/0.84M 11.99 6378 411kt 17.663 112 T-45 Goshawkl x Rolls-Royce Turbomeca F405-401 turbofan5845kW/26kN production 8125 783 42250 990 tandem 1700 1444 (a) (a) ferry, internal fuel only Promavia 9 9.4 13.6 Belgium Jet Squalus 1 x Williams-Rolls FJ44 turbofan 1500 300kt 2500 335 2000 260kt 35000 366 2400 67 720 1500(a) 7.2kN production side-by-side (a) at 20,000ft, max fuel Raytheon Aircraft Beech Mkll JPATSl x Pratt & Whitney Canada PT6A-62 turbopropl270kW(derated to 930kW)production 10.19 1685 320kt/0.68M 4090 227 10.17 3200 38000 417 tandem 58 FLIGHT INTERNATIONAL 1 - 7 November 1995
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