Statements (51)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:engine
|
| gptkbp:bfsLayer |
5
|
| gptkbp:bfsParent |
gptkb:Rotax_engine
gptkb:Rotax_Aircraft_Engines |
| gptkbp:application |
gptkb:aircraft
|
| gptkbp:certification |
EASA and FAA certified
|
| gptkbp:color |
black and silver
|
| gptkbp:compression_ratio |
9.2:1
|
| gptkbp:controls |
Electronic Engine Control (EEC)
|
| gptkbp:cooling_system |
gptkb:fandom
liquid-cooled water-glycol mixture |
| gptkbp:displacement |
141.2 cubic inches
|
| gptkbp:emissions_standard |
dual exhaust
dual air intake |
| gptkbp:engine |
aluminum alloy
lightweight design up to 2000 hours inline configuration flexible mount system 100 hp at 5800 RPM maximum 5800 RPM used in various ultralight and light sport aircraft. |
| gptkbp:engine_type |
horizontally opposed engine
roller camshaft |
| gptkbp:features |
turbocharged
|
| gptkbp:first_introduced |
gptkb:2016
|
| gptkbp:frequency |
200 hours
|
| gptkbp:fuel_capacity |
dry sump
approximately 5.5 gph length 600 mm, width 600 mm, height 500 mm |
| gptkbp:fuel_type |
electronic fuel injection
electric fuel pump MOGAS or AVGAS |
| https://www.w3.org/2000/01/rdf-schema#label |
Rotax 915i S
|
| gptkbp:ignition_system |
gptkb:NGK
dual ignition |
| gptkbp:is_tested_for |
extensively tested for reliability
|
| gptkbp:launch_site |
electric starter
|
| gptkbp:manufacturer |
gptkb:BRP-Rotax
|
| gptkbp:market_segment |
general aviation
|
| gptkbp:max_speed |
5800 RPM
|
| gptkbp:powers |
100 hp
|
| gptkbp:propulsion |
constant speed propeller
|
| gptkbp:setting |
inline four-cylinder
|
| gptkbp:torque |
max torque at 3800 RPM
|
| gptkbp:tuning |
factory tuned
|
| gptkbp:type |
four-stroke engine
|
| gptkbp:valve_configuration |
DOHC
|
| gptkbp:warranty |
2 years or 1000 hours
|
| gptkbp:weight |
approximately 75 kg
|