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Aircraft Design

Aircraft Design. Dassault /Dornier Alpha Jet. Dassault /Dornier Alpha Jet. . General characteristics Crew: 1-2 Length: 13.23 m (43 ft 5 in) Wingspan : 9.11 m (29 ft 10¾ in) Height: 4.19 m (13 ft 9 in) Wing area: 17.50 m² (188.4 ft²) Empty weight : 3,515 kg (7,750 lb )

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Aircraft Design

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  1. Aircraft Design

  2. Dassault/Dornier Alpha Jet

  3. Dassault/Dornier Alpha Jet • . General characteristics • Crew: 1-2 • Length: 13.23 m (43 ft 5 in) • Wingspan: 9.11 m (29 ft 10¾ in) • Height: 4.19 m (13 ft 9 in) • Wing area: 17.50 m² (188.4 ft²) • Empty weight: 3,515 kg (7,750 lb) • Loaded weight: 5,000 kg (11,000 lb) • Max takeoff weight: 7,500 kg (16,535 lb) • Powerplant: 2× SNECMA TurbomecaLarzac 04-C5 turbofans, 13.24 kN (2,976 lbf) each • Performance • Maximum speed: 1,000 km/h (540 kn, 621 mph) at sea level • Stall speed: 167 km/h (90 knots, 104 mph) (flaps and undercarriage down) • Combat radius: 610 km (329 nmi, 379 mi) lo-lo-lo profile, gun pod, underwing weapons and two drop tanks • Ferry range: 2,940 km (1,586 nmi, 1,827 mi) • Service ceiling: 14,630 m (48,000 ft) • Rate of climb: 57 m/s (11,220 ft/min) • Armament • Guns: 1× 27 mm (1.06 in) Mauser BK-27cannon in centreline gun pack • Rockets: 2× Matra rocket pods with 18× SNEB 68 mm rockets each; 2× CRV7 rocket pods with 19× 70 mm rockets each • Missiles: 2× AIM-9 Sidewinders; 2× Matra Magic IIs; 2× AGM-65 Maverick; • Bombs: 2,500 kg (5,500 lb) of payload on five external hardpoints, including a variety of bombs (such as the Hunting BL755cluster bombs) orDrop tanks for extended range.

  4. Yakovlev Yak-130

  5. Yakovlev Yak-130 • General characteristics • Crew: 2 pilots • Length: 11.49 m (37 ft 8 in) • Wingspan: 9.72 m (31 ft 10 in) • Height: 4.76 m (15 ft 7 in) • Wing area: 23.52 m² (253.2 sq ft) • Empty weight: 4,600 kg (10,141 lb) • Loaded weight: 6,350 kg (14,000 lb) • Max takeoff weight: 6,500 kg (14,330 lb) • Powerplant: 2× Klimov-Motor sich AI-222-25 turbofan, 21.58 kN (4,852 lbf) each • Performance • Maximum speed: 1,050 km/h (644 mph) • Cruise speed: 887 km/h (551 mph) • Stall speed: 165 km/h (103 mph) • Range: 2,546 km (1,582 miles) • Service ceiling: 12,500 m (42,660 ft) • Rate of climb: 50 m/s (10,000 ft/min) • Wing loading: 276.4 kg/m² (56.60 lb/sq ft) • Thrust/weight: 0.68 • Armament • Nine hard points for a mixed load of all types of Russian and western air to air (short to medium range) and air to ground dumb and smart bombs [11]

  6. Bae Hawk

  7. Bae Hawk • General characteristics • Crew: 2: student, instructor • Length: 12.43 m (40 ft 9 in) • Wingspan: 9.94 m (32 ft 7 in) • Height: 3.98 m (13 ft 1 in) • Wing area: 16.70 m² (179.64 ft²) • Empty weight: 4,480 kg (9,880 lb) • Useful load: 3,000 kg (6,600 lb) • Max takeoff weight: 9,100 kg (20,000 lb) • Powerplant: 1× Rolls-Royce Adour Mk. 951 turbofan with FADEC, 29 kN (6,500 lbf) 29 kN • Performance • Maximum speed: 0.84 Mach (1,028 km/h, 638 mph) at altitude • Range: 2,520 km (1,360 NM, 1,565 mi) • Service ceiling: 13,565 m (44,500 ft) • Rate of climb: 47 m/s (9,300 ft/min) • Thrust/weight: 0.65 • Armament • Up to 6,800 lb (3,085 kg) of weapons on five hardpoints, including: • 4× AIM-9 Sidewinder or ASRAAM on wing pylons and wingtip rails • 1,500 lb (680 kg), limited to one centreline and two wing pylons (Hawk T1)

  8. HAL HJT-36 SITARA

  9. HAL HJT-36 SITARA • Dimensions: • Length 10.91m • Height 4.13m • Wingspan 9.8m • Weights: • Maximum Take-Off Weight 4,500kg • Take-Off Weight, No External Payload 3,500kg • External Payload 1,000kg • Engines: • Prototype Aircraft • SnecmaLarsac 04-H20, rated 14.12kN • Series Production Aircraft • Saturn AL-55, rated 16.68kN • Fuel 1,150l, 917kg • Performance: • Manoeuvrability +7g to –2.5g • Maximum Operating Speed 960km/h, Mach 0.8 • Maximum Level Speed 700km/h, Mach 0.58 • Maximum Dive Speed 824km.h, Mach 0.69 • Service Ceiling 12,000m • Range 1,000km • Endurance 3 hours

  10. Aero L-39 Albatros

  11. Aero L-39 Albatros • Data from Jane's All The World's Aircraft 1988-89 [9] • General characteristics • Crew: 2 • Length: 12.13 m (39 ft 9½ in) • Wingspan: 9.46 m (31 ft 0½ in) • Height: 4.77 m (15 ft 7¾ in) • Wing area: 18.8 m² (202 ft²) • Airfoil: NACA 64A012 mod • Empty weight: 3,455 kg (7,617 lb) • Max takeoff weight: 4,700 kg (10,362 lb) • Powerplant: 1× Ivchenko AI-25TL turbofan, 16.87 kN (3,792 lbf) • Performance • Never exceed speed:Mach 0.80 (609 mph, 980 km/h) • Maximum speed: 750 km/h (405 knots, 466 mph) at 5,000 m (16,400 ft) • Range: 1,100 km (593 nmi, 683 mi) (internal fuel) • 1,750 km, (944 nmi, 1,087 mi) (internal and external fuel) • Service ceiling: 11,000 m (36,100 ft) • Rate of climb: 13.5 m/s (4,130 ft/min) • Wing loading: 250.0 kg/m² (51.3 lb/ft²) • Thrust/weight: 0.37 • Climb to 5,000 m (16,400 ft): 5 min • Endurance: • 2 hr 30 min (internal fuel) • 3 hr 50 min (internal and external fuel) • Take-off roll: 530 m (1,740 ft) • Landing roll: 650 m (2,140 ft) • Armament • Up to 284 kg (626 lb) of stores on two external hardpoints • 2× wingtip fuel tanks

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