Turbojet Trainer With Reheat

Turbojet Trainer With Reheat

Nett dimensions andweight: 1385 mm (wide) x 1200 mm (depth) x 1721 mm (height) and 260kg
Approximate packeddimensions and weight: 3.8 m3 and 450 kg
Fuel: High-qualityaviation kerosene: ASTM D 1655 Jet A or similar

Gas generatorturbine:
Maximum continuous speed: Approximately 100000 rev.min–1
Approximate maximum thrust:50 N

Instruments:
Shaft speed
Pressures
Temperatures
Fuel flow
Thrust
Nozzle area
Fuel flow level and pressure
Oil temperature and pressure
Filter condition
Total hours run

Automatic shut downconditions:
Ignition failure
Incorrect turbine speed
Oil pressure failure
Water supply failure
Incorrect temperatures

Exhaust emissions(typical):
Carbon dioxide (CO2): 1.8 – 2.9%
Carbon monoxide, (CO): 240 – 900 ppm
Nitric oxide, (NO): 11 – 26 ppm
Nitrogen dioxide, (NO2): 0 – 1 ppm
Combination of NO and NO2, (NOX): 12 – 26 ppm
Sulphur dioxide, (SO2): 5 – 6 ppm