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.
TBS 400N-J40P Technical data
Manufacturer | TBS Schwabhausen GmbH |
Initial testing | |
Certification | |
Type | Single-shaft turbojet |
Nb. built | |
Spools | 1 |
Bearings | Ceramic Hybrid with Squeeze-film Damping |
Compressor | 1R |
Burner | Annular / air blast |
Turbine | Single Stage Axial |
Control | Full Authority Digital |
Dimensions
Diameter | 156 mm | 6.14 in. |
Length overall | 420 mm | 16.54 in. |
Weight
Not equipped | 4 kg | 8.8 lbs |
Equipped | kg | lbs |
Performances
Max RPM | t/mn | rpm |
Idle RPM | t/mn | rpm |
Thrust at max RPM | 420 N | 94.42 lb |
Thrust max continuous | 400 N | 89.92 lb |
Thrust at idle RPM | N | lb |
Pressure ratio | 3.8 / 1 | |
Max Flow | 0.78 kg/s | 1.72 lbs/sec |
Max continue EGT | 720 deg.C | 1328 deg.F |
Consumption
Consumption | ||
Specific fuel consumption | 35 g/kN/s |