Table of contents:
Engine performance datasheets (thrust and fuel flow variation as a function of rotation speed N1, Mach number and altitude) can be downloaded here: Engine Datasheets
The software GasTurb of GasTurb GmbH (http://www.gasturb.de/index.html) has been used to model the CSR-01 thermodynamic engine model.
Definitions and additional explanations can be found under: Parameter Definitions
| Parameter | Unit | Value |
|---|---|---|
| Engine Type | - | 2 x V2527-A5 |
| SLST (Flat rated thrust @ SL/Ma0/ISA+15) | kN | 117.88 |
| lbf | 26500 | |
| Equivalent Thrust (1.25⋅thrust@SL/Ma0.25/ISA+15) | kN | 118.6 |
| lbf | 26671 | |
| Average cruise offtakes | ||
| - Bleed air | kg/s | 0.98 |
| - Shaft power | kW | 52 |
| Parameter | Unit | Max. T/O (SL/Ma0.0/ISA+15) | Bucket Pt. (FL350/Ma0.78/ISA) | Bucket Pt. with offtakes (FL350/Ma0.78/ISA/ Avg. Cruise Offtakes) |
|---|---|---|---|---|
| Thrust | kN | 117.9 | 21.7 | 21.7 |
| lbf | 26500 | 4874 | 4883 | |
| Fuel flow | kg/s | 1.2 | 0.3 | 0.4 |
| TSFC | (g/s)/kN | 9.96 | 16.03 | 16.73 |
| (lb/hr)/lbf | 0.352 | 0.566 | 0.59 | |
| N1 | % | 101.5 | 85.4 | 87.5 |