Statements (51)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:engine
|
| gptkbp:application |
gptkb:aircraft
|
| gptkbp:certification |
EASA certified
|
| gptkbp:compression_ratio |
9.2:1
|
| gptkbp:controls |
ECU
|
| gptkbp:cooling_system |
liquid-cooled
water-cooled |
| gptkbp:displacement |
141.2 cubic inches
|
| gptkbp:emissions_standard |
dual exhaust
|
| gptkbp:engine |
gptkb:4
aluminum alloy high efficiency reliable performance electric start horizontally opposed detailed specifications available multiple aircraft models 100 hp at 5800 RPM popular in aviation community integrated turbocharger engine mount system |
| gptkbp:engine_type |
turbocharged engine
|
| gptkbp:first_introduced |
gptkb:2016
|
| gptkbp:frequency |
200 hours
|
| gptkbp:fuel_capacity |
500 mm
600 mm 400 mm 4.5 liters 10 L/h |
| gptkbp:fuel_type |
aviation gasoline
electronic fuel injection |
| https://www.w3.org/2000/01/rdf-schema#label |
Rotax 915
|
| gptkbp:ignition_system |
gptkb:NGK
dual ignition |
| gptkbp:is_tested_for |
bench tested
|
| gptkbp:maintenance |
easy maintenance
|
| gptkbp:manufacturer |
gptkb:BRP-Rotax
|
| gptkbp:max_speed |
5800 RPM
|
| gptkbp:operational_range |
up to 25,000 feet
|
| gptkbp:power_output |
100 hp
|
| gptkbp:propulsion |
constant speed propeller
|
| gptkbp:setting |
inline-four
|
| gptkbp:torque |
135 Nm
wet sump 135 Nm at 5000 RPM |
| gptkbp:type |
four-stroke engine
|
| gptkbp:valve_configuration |
DOHC
|
| gptkbp:warranty |
2 years
|
| gptkbp:weight |
75 kg
|
| gptkbp:bfsParent |
gptkb:Rotax
|
| gptkbp:bfsLayer |
5
|