DeltaHawk DH180A4
| DH180A4 | |
|---|---|
| Type | Water-cooled V-four diesel piston aircraft engine |
| National origin | United States |
| Manufacturer | DeltaHawk Engines, Inc. |
| First run | 1997 |
| Major applications | Cirrus SR20 |
|
| |
The DH180A4 is V-4 diesel piston aircraft engine developed for aircraft applications by DeltaHawk.
In 2014, a DH180A4 was installed and demonstrated at the EAA Airventure airshow on a Cirrus SR20. A retrofit kit is planned for the SR20.[1]
Variants
- DH160A4/V4/R4 160 hp V-4
- DH180A4/V4/R4 180 hp V-4
- DH200A4/V4/R4 200 hp V-4
Applications
Specifications (DH180A4)
General characteristics
- Type: Four-cylinder water-cooled piston
- Dry weight: 327 lb
Components
- Fuel type: jet-A, jet-A1,JP-5, JP-8, Diesel #1, Diesel #2, bio-diesel
- Cooling system: water cooled
Performance
- Power output: 180 hp (134 kW) @ 3600 rpm
- Specific fuel consumption: .39 lb/hp/hr
References
- ↑ Jim Moore (March 2015). "Diesels on the cusp". AOPA Pilot: 87.
External links
This article is issued from Wikipedia - version of the Saturday, July 11, 2015. The text is available under the Creative Commons Attribution/Share Alike but additional terms may apply for the media files.