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) Loaded weight: 5,000 kg (11,000 lb) Max takeoff weight: 7,500 kg (16,535 lb) Powerplant: 2× SNECMA Turbomeca Larzac 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-27 cannon 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 BL755 cluster bombs) or Drop tanks for extended range.

Yakovlev Yak-130

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]

Bae Hawk

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)

HAL HJT-36 SITARA

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 Snecma Larsac 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

Aero L-39 Albatros

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