silentinksoldier
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While Mi17s have done the job well for the IAF, it cant be denied that the chopper DOES have ceratin shortcomings. For one, it isnt very maneuverable or agile.
While it does have a high troop load, and is obviously the perfect choice for bringing in additional troops to the frontlines once a certain degree of superiority has been achieved, it might not be the best choice for exectuting drops at hot LZs.
Should india be looking at another chopper to supplement the hip in this role? If so, which chopper would fulfil our needs?
We could take a look at the Nh-90.
specs:
Crew: 2 pilots (and possible sensor operator on NFH)
Capacity: 20 troops/12 stretchers/2 NATO Pallets
Length: 16.13 m (52 ft 11 in)
Rotor diameter: 16.30 m (53 ft 6 in)
Height: 5.23 m (17 ft 2 in)
Empty weight: 6,400 kg (14,100 lb)
Useful load: 4,200 kg (9,260 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
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)
While it does have a high troop load, and is obviously the perfect choice for bringing in additional troops to the frontlines once a certain degree of superiority has been achieved, it might not be the best choice for exectuting drops at hot LZs.
Should india be looking at another chopper to supplement the hip in this role? If so, which chopper would fulfil our needs?
We could take a look at the Nh-90.
specs:
Crew: 2 pilots (and possible sensor operator on NFH)
Capacity: 20 troops/12 stretchers/2 NATO Pallets
Length: 16.13 m (52 ft 11 in)
Rotor diameter: 16.30 m (53 ft 6 in)
Height: 5.23 m (17 ft 2 in)
Empty weight: 6,400 kg (14,100 lb)
Useful load: 4,200 kg (9,260 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
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)
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