Breaking News:
22.08.2012
La saga des BD-5J
Entre le 15 mai et le 1er août 2012, 3 nouveaux BD-5J ont fait leur premier vol.Aux Etats Unis...
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. Thrust | 400 N |
Thrust to Weight Ratio | 10.5 |
SFC | 35g /kNs |
Mass Flow | 0.78kg/ s |
EGT red line | 720 °C |
Pressure Ratio | 3.8 |
Characterisitics
Spools | 1 |
Bearings | Ceramic Hybrid with Squeeze-film Damping |
Compressor | 1R |
Burner | Annular / air blast |
Turbine | Single Stage Axial |
Control | Full Authority Digital |
