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Post by Rosaria on Feb 5, 2019 16:40:26 GMT
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Post by Rosaria on Feb 5, 2019 16:49:42 GMT
Aircraft
U/AV-17 Hawk: $86,000,000 per unit
Crew: Four (pilot, copilot and two flight engineers/crew chiefs)
Capacity:
14 troops (seated), 22 troops (floor loaded), or
15,000 lb of internal cargo, or up to 10,000 lb of external cargo (dual hook)
1× light internally transportable ground vehicle[287][288]
Length: 47 ft 4 in (17.5 m)
Rotor diameter: 38 ft 0 in (11.6 m)
Wingspan: 45 ft 10 in (14 m)
Width with rotors: 84 ft 7 in (25.8 m)
Height: 22 ft 1 in/6.73 m; overall with nacelles vertical (17 ft 11 in/5.5 m; at top of tailfins)
Disc area: 2,268 ft² (212 m²)
Wing area: 301.4 ft² (28 m²)
Empty weight: 33,140 lb (15,032 kg)
Loaded weight: 47,500 lb (21,500 kg)
Max. takeoff weight: 50,500 lb (27,400 kg) (self-deploy/long runway)
Maximum rolling takeoff weight: 47,000 lb (STOL)
Maximum vertical takeoff weight: 42,600 lb[51]
Maximum speed: 275 knots (509 km/h, 316 mph[289]) at sea level / 305 kn (565 km/h; 351 mph) at 15,000 ft
Cruise speed: 241 kn (277 mph, 446 km/h) at sea level
Stall speed: 110 kn[74] (126 mph, 204 km/h) in airplane mode
Range: 679 nmi
Combat radius: 320 nmi
Ferry range: 1,940 nmi (2,230 mi, 3,590 km) with auxiliary internal fuel tanks
Service ceiling: 25,000 ft (7,620 m)
Rate of climb: 2,320–4,000[74] ft/min (11.8 m/s)
Glide ratio: 4.5:1[74]
Disc loading: 20.9 lb/ft² at 47,500 lb GW (102.23 kg/m²)
Power/mass: 0.259 hp/lb (427 W/kg)
Armament
2× 6.5mm x 75mm dual nose turret
1 x 6.5mm x 75mm door mounted MG
TT-103: $22,000,000 per unit
Crew: Five: 2 pilots, 1 navigator, 1 flight engineer, 1 flight technician
Capacity:
90 troops or 60 stretchers
20,000 kg cargo
Length: 40.025 m
Height: 8.145 m
Empty weight: 28,200 kg
Loaded weight: 49,600 kg
Max. takeoff weight: 56,000 kg
Powerplant: 2 × Lotarev D-136 AI-136 (or PD-12V altpw) turboshafts, 8,500 kW (10-11,398 shp or ~ 10-12,000 of PD12V) each
Performance
Maximum speed: 295 km/h
Cruise speed: 255 km/h
Range: 800 km
Ferry range: 1,920 km
Service ceiling: 4,600 m
VS-212: $32,000,000 per unit
Crew: 2 pilots (and possible sensor operator on NFH)
Capacity: 20 seated troops; or 12 medevac stretchers; or 2 Supply pallets; or 4,200 kg
Length: 16.13 m
Rotor diameter: 16.30 m
Height: 5.23 m
Empty weight: 6,400 kg
Useful load: 4,200 kg
Max. takeoff weight: 10,600 kg
Powerplant: 2 × Rolls-Royce Turbomeca RTM322-01/9 turboshaft
Performance
Maximum speed: 300 km/h
Range: 800 km (497 mi) TTH
1,000 km (621 mi) NFH
Service ceiling: 6,000 m
Rate of climb: 8 m/s
Armament
Guns: 2x door gun
Missiles: anti-submarine and/or air to surface missiles (NFH version)
A-21: $235,000,000 per unit
Crew: 7 typical (aircraft commander, pilot, two flight engineers, three loadmasters)
4 minimum (pilot, copilot, two flight engineers)
Payload: 270,000 lb
Length: 247 ft 1 in
Wingspan: 222 ft 9 in
Height: 65 ft 1 in
Empty weight: 380,000 lb
Useful load: 389,000 lb
Loaded weight: 769,000 lb
Max. takeoff weight: 840,000 lb
Powerplant: 4 × General Electric TF39-GE-1C high-bypass turbofan, 43,000 lbf (190 kN) each
Performance
Maximum speed: Mach 0.79
Cruise speed: Mach 0.77
Range: 2,400 nmi (2,760 mi, 4,440 km) with a 263,200 lb (119,400 kg) payload
Service ceiling: 35,700 ft (10,600 m) at 615,000 lb (279,000 kg) gross weight
Rate of climb: 1,800 ft/min
Thrust/weight: 0.22
Takeoff roll: 8,400 ft
Landing roll: 3,600 ft
Fuel capacity: 51,150 US gal
A-500: $75,000,000 per unit
Crew: 6
Length: 84 m
Wingspan: 88.4 m
Height: 18.1 m
Empty weight: 285,000 kg
Max takeoff weight: 640,000 kg
Fuel capacity: 300,000 kg
Powerplant: 6 × Progress D-18T turbofans, 229.5 kN (51,600 lbf) thrust each
Performance
Maximum speed: 850 km/h
Cruise speed: 800 km/h
Range: 15,400 km
Service ceiling: 11,000 m
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