- Reaction score
- 79
- Points
- 680
Specs for the EH101 and the CH149 are identical (at least to me)
Specifications (Merlin HM1)
Crew: 4
Capacity:
24 seated troops or
45 standing troops or
16 stretchers with medics
Length: 22.81 m (74 ft 10 in)
Rotor diameter: 18.59 m (61 ft 0 in)
Height: 6.65 m (21 ft 10 in)
Disc area: 271 m² (2,992 ft²)
Empty weight: 10,500 kg (23,150 lb)
Useful load: 5,443 kg (12,000 lb)
Max takeoff weight: 15,600 kg (32,188 lb)
Powerplant: 3× Rolls-Royce/Turbomeca RTM322-01 turboshafts, 1,725 kW (2,312 shp) each
Performance
Never exceed speed: 309 km/h (167 knots, 192 mph)
Range: 1,389 km (750 nm, 863 mi)
Service ceiling 4,575 m (15,000ft)
Rate of climb: 10.2 m/s (2,000 ft/min)
Disc loading: 53.8 kg/m² (11.01 lb/ft²)
Power/mass: 284.9 W/kg (0.174 shp/lb)
General characteristics
Crew: 5
1-Aircraft Commander, 1-First Officer, 1-Flight Engineer, 2-SAR Techs
Capacity:
30 seated troops or
45 standing troops or
16 stretchers with medics
Length: 74 ft 10 in (22.81 m)
Rotor diameter: 61 ft 0 in (18.59 m)
Height: 21 ft 10 in (6.65 m)
Disc area: 2992 ft² (271 m²)
Empty weight: 23,150 lb (10,500 kg)
Useful load: 5,443 kg (12,000 lb)
Max takeoff weight: 32,188 lb (14,600 kg)
Powerplant: 3× General Electric T700-T6A1 turboshafts, 1,723 shp (1286 kW) each
Performance
Never exceed speed: 167 knots (192 mph, 309 km/h)
Range: 750 nm (863 mi, 1389 km)
Service ceiling 15,000ft (4575 m)
Rate of climb: 2000 ft/min (10.2 m/s)
Disc loading: 53.8 kg/m² (11.01 lb/ft²)
Power/mass: 0.174 shp/lb (284.9 W/kg)
So shouldn't the parts be interchangable?
Specifications (Merlin HM1)
Crew: 4
Capacity:
24 seated troops or
45 standing troops or
16 stretchers with medics
Length: 22.81 m (74 ft 10 in)
Rotor diameter: 18.59 m (61 ft 0 in)
Height: 6.65 m (21 ft 10 in)
Disc area: 271 m² (2,992 ft²)
Empty weight: 10,500 kg (23,150 lb)
Useful load: 5,443 kg (12,000 lb)
Max takeoff weight: 15,600 kg (32,188 lb)
Powerplant: 3× Rolls-Royce/Turbomeca RTM322-01 turboshafts, 1,725 kW (2,312 shp) each
Performance
Never exceed speed: 309 km/h (167 knots, 192 mph)
Range: 1,389 km (750 nm, 863 mi)
Service ceiling 4,575 m (15,000ft)
Rate of climb: 10.2 m/s (2,000 ft/min)
Disc loading: 53.8 kg/m² (11.01 lb/ft²)
Power/mass: 284.9 W/kg (0.174 shp/lb)
General characteristics
Crew: 5
1-Aircraft Commander, 1-First Officer, 1-Flight Engineer, 2-SAR Techs
Capacity:
30 seated troops or
45 standing troops or
16 stretchers with medics
Length: 74 ft 10 in (22.81 m)
Rotor diameter: 61 ft 0 in (18.59 m)
Height: 21 ft 10 in (6.65 m)
Disc area: 2992 ft² (271 m²)
Empty weight: 23,150 lb (10,500 kg)
Useful load: 5,443 kg (12,000 lb)
Max takeoff weight: 32,188 lb (14,600 kg)
Powerplant: 3× General Electric T700-T6A1 turboshafts, 1,723 shp (1286 kW) each
Performance
Never exceed speed: 167 knots (192 mph, 309 km/h)
Range: 750 nm (863 mi, 1389 km)
Service ceiling 15,000ft (4575 m)
Rate of climb: 2000 ft/min (10.2 m/s)
Disc loading: 53.8 kg/m² (11.01 lb/ft²)
Power/mass: 0.174 shp/lb (284.9 W/kg)
So shouldn't the parts be interchangable?