Crusader2000
Banned Member
Well, here are the spec for the NH-90 vs the H-92 and Naval CH-148. Seem very close to me? Plus, the fact the latter two share a great deal with the UH-60 Blackhawk and SH-60 Seahawk!
Specifications
NH-90
General characteristics
Crew: 2 pilots (and possible sensor operator on NFH)
Capacity: 20 troops/12 stretchers
Length: 16.13 m (52 ft 11 in)
Rotor diameter: 16.30 m (53 ft 5¾ in)
Height: 5.23 m (17 ft 2 in)
Empty weight: 5,400 kg (11,900 lb)
Max takeoff weight: 10,600 kg (23,370 lb)
Powerplant: 2× Rolls-Royce Turbomeca RTM322-01/9 turboshaft, 1,662 kW (2,230 shp) each, or:
Powerplant: 2× General Electric T700-T6E turboshafts, 1,577 kW (2,115 shp) each
Performance
Maximum speed: 300 km/h (162 knots, 186 mph)
Range: 800 km, 497 mi (TTH); 1,000 km, 621 mi (NFH) ()
Service ceiling: 6,000 m (20,000 ft)
Rate of climb: 480 m/min (1,574 ft/m)
__________________________________________________________________________
S/H-92
General characteristics
Crew: 3 (pilot, co-pilot, observer)
Capacity: 19 passengers
Length: 56 ft 2 in (17.10 m)
Rotor diameter: 56 ft 4 in (17.17 m)
Height: 15 ft 5 in (4.71 m)
Disc area: 2,650 ft² (246 m²)
Empty weight: 15,500 lb (7,030 kg)
Loaded weight: 26,500 lb (12,020 kg)
Max takeoff weight: 26,500 lb (12,020 kg)
Powerplant: 2× General Electric CT7-8A turboshaft, 2,740 shp (2,043 kW) each
Fuselage length: 56 ft 2 in (17.1 m)
Fuselage width: 17 ft 3 in (5.26 m)
Rotor systems: 4 blades on main rotor
Performance
Maximum speed: 165 knots (190 mph, 306 km/h)
Cruise speed: 151 kt, 174 mph (280 km/h)
Range: 539 nmi (999 km)
Service ceiling: 14,000 ft (4,270 m)
Disc loading: 9.8 lb/ft² (48 kg/m²)
Power/mass: 0.23 hp/lb (0.38 W/kg)
CH-148 (Naval S-92)
General characteristics
Crew: 4 (2 pilots, 1 tactical officer, 1 sensor operator)
Capacity: 6 in mission config, up to 22 in utility config
Length: 68 ft 6 in (S-92) (20.9 m (S-92))
Rotor diameter: 58 ft 1 in (S-92) (17.7 m (S-92))
Height: 15 ft 5 in (S-92) (4.7 m (S-92))
Disc area: 2,650 ft² (S-92) (246 m² (S-92))
Max takeoff weight: 28,650 lbs (12,993 Kg)
Powerplant: 2× General Electric CT7-8A turboshaft, 3,000 shp (2,238 kW) each
Fuselage length: 56 ft 2 in (17.1 m)
Fuselage width: 17 ft 3 in (5.26 m)
Performance
Maximum speed: 165 knots (190 mph, 306 km/h)
Cruise speed: 137 knots (158 mph, 254 km/h)
Service ceiling: 15,000 ft (4,572 m)
Specifications
NH-90
General characteristics
Crew: 2 pilots (and possible sensor operator on NFH)
Capacity: 20 troops/12 stretchers
Length: 16.13 m (52 ft 11 in)
Rotor diameter: 16.30 m (53 ft 5¾ in)
Height: 5.23 m (17 ft 2 in)
Empty weight: 5,400 kg (11,900 lb)
Max takeoff weight: 10,600 kg (23,370 lb)
Powerplant: 2× Rolls-Royce Turbomeca RTM322-01/9 turboshaft, 1,662 kW (2,230 shp) each, or:
Powerplant: 2× General Electric T700-T6E turboshafts, 1,577 kW (2,115 shp) each
Performance
Maximum speed: 300 km/h (162 knots, 186 mph)
Range: 800 km, 497 mi (TTH); 1,000 km, 621 mi (NFH) ()
Service ceiling: 6,000 m (20,000 ft)
Rate of climb: 480 m/min (1,574 ft/m)
__________________________________________________________________________
S/H-92
General characteristics
Crew: 3 (pilot, co-pilot, observer)
Capacity: 19 passengers
Length: 56 ft 2 in (17.10 m)
Rotor diameter: 56 ft 4 in (17.17 m)
Height: 15 ft 5 in (4.71 m)
Disc area: 2,650 ft² (246 m²)
Empty weight: 15,500 lb (7,030 kg)
Loaded weight: 26,500 lb (12,020 kg)
Max takeoff weight: 26,500 lb (12,020 kg)
Powerplant: 2× General Electric CT7-8A turboshaft, 2,740 shp (2,043 kW) each
Fuselage length: 56 ft 2 in (17.1 m)
Fuselage width: 17 ft 3 in (5.26 m)
Rotor systems: 4 blades on main rotor
Performance
Maximum speed: 165 knots (190 mph, 306 km/h)
Cruise speed: 151 kt, 174 mph (280 km/h)
Range: 539 nmi (999 km)
Service ceiling: 14,000 ft (4,270 m)
Disc loading: 9.8 lb/ft² (48 kg/m²)
Power/mass: 0.23 hp/lb (0.38 W/kg)
CH-148 (Naval S-92)
General characteristics
Crew: 4 (2 pilots, 1 tactical officer, 1 sensor operator)
Capacity: 6 in mission config, up to 22 in utility config
Length: 68 ft 6 in (S-92) (20.9 m (S-92))
Rotor diameter: 58 ft 1 in (S-92) (17.7 m (S-92))
Height: 15 ft 5 in (S-92) (4.7 m (S-92))
Disc area: 2,650 ft² (S-92) (246 m² (S-92))
Max takeoff weight: 28,650 lbs (12,993 Kg)
Powerplant: 2× General Electric CT7-8A turboshaft, 3,000 shp (2,238 kW) each
Fuselage length: 56 ft 2 in (17.1 m)
Fuselage width: 17 ft 3 in (5.26 m)
Performance
Maximum speed: 165 knots (190 mph, 306 km/h)
Cruise speed: 137 knots (158 mph, 254 km/h)
Service ceiling: 15,000 ft (4,572 m)