1. United States
  2. Aircraft
  3. T-34C Turbo Mentor

Basic Information

Category Fixed Wing Type Trainer
Year Commissioned 1977 Year Decommissioned 2013
Agility 1 Damage Points (DP) 3
Empty Weight 1342 kg Max Weight 2494 kg
Runway Information 250-450m (STOL) TOD/LAD Physical Size Small Aircraft (0-12m)
Cost 0 Hypothetical No
Payload Weight 544 kg Crew 1 people

Aircraft Capabilities

Bombsight - Ballistic Computing

Sensor Parameters

Model Purpose Range Scan Interval Generation
No Data

Sensor Coverage Diagram
Model Detection Angle Omnidirectional
No Data

Weapon Loadouts Click to Expand Beta

Loadout Type Role Ready Time Combat Radius
No Data
No Data
No Data
No Data

Signatures

Type Front Side Rear
Visual Detection Range 2.99 nm 5.28 nm 2.99 nm
Visual Classification Range 1.41 nm 2.62 nm 2.19 nm
Infrared Detection Range 1.99 nm 5.47 nm 11.21 nm
Infrared Classification Range 1.17 nm 2.18 nm 1.17 nm
Radar, A-D Band (30-2000 MHz) 1.8 dBsm (1.51 m²) 4.3 dBsm (2.69 m²) 1.8 dBsm (1.51 m²)
Radar, E-M Band (2-100 GHz) 1.8 dBsm (1.51 m²) 4.3 dBsm (2.69 m²) 1.8 dBsm (1.51 m²)

Default Configuration

Model Comments
No Data

Datalink

Type Model Range Channels
Radio UHF/VHF Radio [Unsecure] 100 nm 0

Engines

Model Type Engine Count Military Thrust Afterburner Thrust Military Fuel Rate (SFC) Afterburner Fuel Rate (SFC) Hypothetical Comments
1x PT6A-25 Turboprop 1 715 - 0.63 - No -

Fuel

Fuel Type Fuel Capacity
Aviation Fuel 430