Rotax 915 iS
Rotax 915 iS | |
---|---|
Type | Aircraft engine |
National origin | Austria |
Manufacturer | Rotax |
First run | 2014 |
Major applications | Issoire APM 41 Simba 915iS |
Produced | Expected second half of 2017[1] |
Number built | Prototypes only (2015) |
The Rotax 915 iS is an Austrian aircraft engine, under development by Rotax of Gunskirchen for use in ultralight aircraft, homebuilt aircraft, light-sport aircraft, small helicopters and gyroplanes. The intention is that the engine will eventually be type certified.[2][3]
The engine was first publicly displayed at AirVenture in July 2015[2] and first flown in March 2016.[4]
In January 2016 the engine was named AVweb's "Best New Engine" of 2015.[5]
Design and development
The Rotax 915 iS is a four-cylinder four-stroke, horizontally-opposed, turbocharged, air and liquid-cooled, gasoline engine design, with a mechanical gearbox reduction drive. The turbocharger has a compression ratio of 3.5:1 and the engine will have a critical altitude of 15,000 ft (4,572 m). It employs dual electronically controlled fuel injection, using dual channel Rockwell Collins ECUs, with dual ignition and produces 135 hp (101 kW).[2]
The engine is based on the Rotax 912, but differs in that it has a reinforced crankshaft, new pistons, a new gearbox and a turbocharger. Time between overhauls is expected to be 2000 hours from introduction.[2][6]
The engine can produce rated power up to 15,000 ft (4,572 m) and has a ceiling of 23,000 ft (7,010 m).[6]
Availability is expected for second half of 2017[1].
Applications
Specifications (915 iS)
Data from AVweb[2] and manufacturer's website[1]
General characteristics
- Type: four-cylinder, four-stroke, horizontally-opposed, geared aircraft engine
- Dry weight: 84 kg (185.2 lb) dry
Components
- Turbocharger: with a compression ratio of 3.5:1
- Fuel system: dual channel Rockwell Collins ECUs
- Fuel type: high-octane automotive gasoline
- Cooling system: liquid and air
- Reduction gear: mechanical gear type
Performance
- Power output: 135 hp (101 kW)
- Specific fuel consumption: 280 – 310 g/(kW·h) at 5,500 rpm
- Power-to-weight ratio: 0.73 hp/lb (1.19 kW/kg)
See also
Related lists
References
- 1 2 3 "ROTAX 915 IS/ISC - Rotax Aircraft Engines". www.flyrotax.com. Retrieved 21 August 2017.
- 1 2 3 4 5 "Rotax Announces New 135-hp Turbocharged Engine". AVweb. Retrieved 22 July 2015.
- ↑ "Rotax-Owner.com - ROTAX 915 IS: BRP UNVEILS A NEW TURBOCHARGED ROTAX AIRCRAFT ENGINE". Rotax-Owner. Retrieved 22 July 2015.
- ↑ "Rotax Updates 915iS Progress". AVweb. Retrieved 7 April 2016.
- ↑ "AVweb's Stuff of the Year". AVweb. Retrieved 2 January 2016.
- 1 2 "Rotax 915iS Sport Moves Closer To Market". AVweb. Retrieved 28 July 2016.