| Aircraft Engine Manufacturer |
Microturbo |
Power Jets |
| Aircraft Engine Type |
Turbojet |
Turbojet |
| Dry Weight (kg) |
61.2 |
|
| Diameter (mm) |
343 |
1143 |
| Length (mm) |
841 |
1706.88 |
| Wikipedia Article (URL) |
en.wikipedia.org/wiki/Microturbo_TRI_60 |
en.wikipedia.org/wiki/Power_Jets_WU |
| Fuel |
|
Kerosene |
| Geared Fan |
No |
No |
| Combustion Chamber |
annular |
single straight through design, located immediately downstream of elbow in spiral pipe |
| Afterburner |
No |
No |
| Streams |
1 |
1 |
| Maximum Takeoff Thrust (kN) |
5.7 |
6.18 |
| Thrust To Weight |
9.53 |
|
| Compressor Description |
4 stage axial |
single-stage centrifugal with 19-inch diameter double-sided impeller, diffuser vanes installed part way through testing, material: Hiduminium RR 56 |
| Turbine Description |
single stage |
14-inch diameter with 66 blades (BTH non-vortex design), single stage axial flow, with no nozzle guide vanes, material of disc and blades: Firth-Vickers Stayblade |