MTA Project envisages development and manfacture of 15-20 Ton Cargo Transport Aircraft for use by Defence/Civil Operators for
transporting Cargo, Armed Personnel & Para-dropping etc. The broad performance parameters of the aircraft are given below,
Maximum Payload | 20000 kg |
Payload Range | 15000-20000 kg |
Maximum Take Off Weight | 68000 kg |
Cruise Speed | 800 km/hr |
Cruise Altitude | 11 km |
Range | 2500-6000 km with different payload
|
Calendar Life | 35 years |
Operational Life | 60000 hrs |
Specification of the MTA have been defined by the Indian Air Force and Russian Air Force.