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TBS 400N-J40P

This engine was developed for HpH by former MTU Engineers and is based upon a well proven military powerplant currently in service. It's size, weight, thrust and fuel consumption have been tailored especially for use in a glider.

Performances

Max. thrust 420 N 
Rated max. Thrust400 N 
Thrust to Weight Ratio10.5 
SFC 35 g/kNs 
Mass Flow 0.78 kg/s 
EGT red line 720 °C 
Pressure Ratio3.8

Characteristics

Spools1
BearingsCeramic Hybrid with Squeeze-film Damping
Compressor1R
BurnerAnnular / air blast
TurbineSingle Stage Axial
ControlFull Authority Digital
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