Performance
Continental Diesel CD-155 (155 hp)
Continental Diesel offers with the CD-155 a jet fuel piston engine for general aviation with a take off power of 99 kW (155 hp). The CD155 is a turbo charged 4-cylinder in-line engine. The CD-155 is certified for the use of both jet fuel and diesel (DIN EN590) and is running with the two fuels in any mixture ratio.The engine has a time between replacement (TBR) of 2100 hr. Despite of improved performance, the CD-155 weighs as much as the CD-135.
General Engine Description
| Engine work principle: | Turbo diesel engine | |
| Cylinder, Configuration: | 4, in-line | |
| Intake system: | Common rail direct injection | |
| Cooling: | Liquid cooled | |
| Approved propeller: | 3-blade propeller of MT with hydraulic variable pitch (MTV-6 series) | |
| Weight (complete & dry): | 134 kg | 295.4 lbs |
| Usable Fuels (UAV): | Diesel (EN 590), Jet A, Jet A-1, JP-5, DEF STAN 91-86, JP-8, DEF STAN 91-91, JP-8+100, Chinese Jet Fuel No 3 |
Performance
| Max. Power up to 6,000ft: | 114 kW | 155 hp |
| Max. Continuous Power: | 114 kW | 155 hp |
| Power Best Economy: | 97 kW | 132 hp |
| Recommended Load: | 75 percent | |
| Power constant: | available max. power at respective altitude | |
| Consumption in cruise flight: | 18-22 l/h | 4.7-5.8 gal/hr |