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Aviation History
1995
1995 - 3152.PDF
MILITARY AIRCRAFT OF THE WORLD 14 RFB 9.7 9.6 14 Rockwell 10.5 10.9 15.5 Siai-Marchetti SRL 8.46 9.53 12.6 Sukhoi 14.36 1160 2300 DASA 2814 3946 4445 2030 2900 4000 9500 15.53 14600-17,600 33.7 WSK PZL-Mielec 9.6 13.2 19.9 GSz-23, 23mm bore, WSK PZL-Mielec 9.6 13.2 19.9 GSz-23, 23mm bore WSK PZL-Mielec 10.83 13.2 23.01 GSz-2-30mm, AAMs, WSK PZL-Mielec 10.83 13.2 23.01 30mm gun, rockets, WSK PZL-Mielec 9.6 13.2 19.9 19500 4730 8600 61 Germany 338kt 300kt 61 USA, GermanyRc 330kt/0.7M 165kt/0.56M 81.4 Italy 414kt/0.8M 88 480 1040 (a) Tiro-Trainer 1 x Williams-Rolls FJ44 turboprop 3169 230 250900 25 480 1180 (a) ckwell/DASA Ranger 20001 x Pratt & Whitney Canada JT 3900 627 40000 858 927 1585 6.78kN 2h development tandem L5D-5C turbofanll.94kN prototype 4/6 S.211A1 x Pratt & Whitney Canada JT15D-5C turbofan 14.19kN 5100 440 42000 415 893 2680 (a RussiaSu-25UT Frogfoot B 2 x Soyuz R-195 turbojets 975W/0.8M Poland 495W/0.8M 500kt 110.3 600 22965 400 ('chute) 2500 (a) Iryda M-93 K 2 x WSK PZL-Rzeszow K-15 turbojet 9055 670 (clean) 4h 15mins (a) 780 (b) 88.4kN 14.7kN 2hrs 30mins (b) 41010 440 (clean)200 -350 depends on load 2430 1200 (a) S-5 57mm, R-60 (AA-8 Aphid), 50,100, 250 & 500kg bombs, Saturn & Fobos recce pod 4570 8600 Poland 495W/0.82M 500kt 109.7 Iryda M-93 V 2 x Rolls-Royce Viper 545 turbojets 8860 670 (clean) : 43470 440 (clean)200 2430 1200 (a) S-5 57mm, R-60 (AA-8 Aphid), 50.100, 250 & 500kg bombs, Saturn & Fobos recce pod 5410 12300 Poland 495W/0.95M 500kt 91.89 ASMs, bombs <l,000kg, recce 5170 12100 AAMs, ASMs 4670 6900 Poland 495M/0.95M 500kt 91.89 bombs <1000kg Poland 495W/0.8M 500M 112 M-99A Orkan 2 x Rolls-Royce Adour 871 turbofans 15550 250 (clean) 47570 290 (clean) 3600 2400 (a) pods, smart weapons pods M-99S 0rkan2 x Povazske Strojavne DV-2A turbofans 12795 250 (clean) 47243 270 (clean)300 3600 2400 (a) recce pods, smart weapons pods. PZL1-22 Iryda 2 x WSK PZL-Rzeszow PZL-5 turbojet 1800 14.73kN hrs 30 mins (b) 350 depends on load 1800 26.76kN 300 (b) 4000 25kN 600km depending on 4000 10.79kN 7280 1130 clean2hr 35 mins clean config 39370 440 clean200 -250 depends on load 2430 1250 (a) GSz-23, 23mm bore. S5 57mm, R-60 (AA-8 Aphid), 50,100, 250 & 500kg bombs, Saturn & Fobos recce pod llMi'l'lll'lil'Mii Atlas Aviation 10.8 10.8 18 IsM'WWH 1545 2200 2750 Daewoo Heavy Industries 10.1 10.3 15.5 Embraer 11.14 9.86 19.4 Embraer 11.42 10.53 19.4 ENAER 8.8 8.4 13.7 Fuji Heavy Industries 10.04 1430 2480 1870 2550 3175 South Africa 300kt 240kt 70 Korea (South) 350kt/0.74M 310M/0.66M 68 1100 Atlas ACE1 x Pratt & Whitney Canada PT6A-34A turboprop 559kW 2750 420 (to 50ft) 5h 30min (a) 36000 430 (from 50ft) 2035 (a) tandem production 5 tandem production tandem production 4 production 4 production 6+2+3 single seat production 116+2+3 load single seat production 4 tandem prototype tandem KTX-11 x Pratt & Whitney Canada PT6A-62 turboprop708kW flat rated from 857kW350 3500 396 38000 512 618 1700 2h 30min (a) 4 tandem 520 7.62mm gun, 70mm rocket BrazilEMB-312 Tucanol x Pratt & Whitney Canada PT6A-25C turboprop 559kW 280kt 222kt 72 2231 380 30000 37 694 1843 (a) BrazilEMB-312H Super Tucanol x Pratt & Whitney Canada PT6A-68-5 turboprop 2420 3190 945 1340 1082 301kt 286kt 85 ChileT- 230kt 182kt 66 Japan 193kt 2925 350 35000 55 694 1568 (a) 35 DT Pillan Turbo 1 x Allison 250-B17D turboprop 2200 195 26500 128 310 556 (a) T-5 1 x Allison 250-B17D turboprop 1700 302 5h(a) 932kW 6h 40min (b) 312kW 4h 30mins 261kW production tandem 3 production tandem development tandem production (a) max internal fuel, at 10,000ft, 45min reserves two demonstrator aircraft based at Rockwell/North American Aircraft Tulsa, Oklahoma site, (a) two wet stations available on request (a) 10% reserves with external fuel; (b) external fuel, 1 gun, 2 rocket launchers. Load factor +7G - 3.5G, sustained load factor si 4.2G (a) ferry, (b) 2 ext tanks time to height 3 min to 6km; (a) 1,879km with underwing tanks; (b) without underwing tanks (a) 1,870km with underwing tanks; (b) without underwing tanks (a) 4,000km with underwing tanks; (b) 600km with underwing tanks (a) 4,00km with underwing tanks (a) max internal fuel (a) at 25,000ft development (a) internal fuel (a) 20,000ft. 30min reserves; (b) 20,000ft Omin reserves, econ cruise (a) at 30.000ft. 30min reserves, (b) max int fuel, econ cruise speed (a) is at 75% power, 45mins reserve FLIGHT INTERNATIONAL 1 - 7 November 1995 59
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