Statements (52)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:jet_engine
|
| gptkbp:application |
gptkb:drones
Experimental Aircraft Ultralight Aircraft Lighter-than-air Aircraft Motor Gliders |
| gptkbp:cooling_system |
Air-cooled
Liquid-cooled |
| gptkbp:country_of_origin |
gptkb:Austria
|
| gptkbp:engine_configuration |
Horizontally Opposed
V-type Engine |
| gptkbp:engine_displacement |
Varies by model
|
| gptkbp:first_introduced |
gptkb:1959
|
| gptkbp:fuel_type |
gptkb:Av_Gas
MOGAS |
| gptkbp:history |
Founded in 1920
Expanded product line in 1990s Acquired by Bombardier in 1970 Became part of BRP in 2003 Introduced 912 series in 1989 |
| https://www.w3.org/2000/01/rdf-schema#label |
Rotax Aircraft Engines
|
| gptkbp:ignition_system |
Electronic Ignition
|
| gptkbp:maintenance |
100 hours
|
| gptkbp:manufacturer |
gptkb:BRP-Rotax
|
| gptkbp:market_segment |
gptkb:General_Aviation
Commercial Aviation Recreational Aviation Sport Aviation |
| gptkbp:notable_models |
gptkb:Rotax_582
gptkb:Rotax_915i_S gptkb:Rotax_914 gptkb:Rotax_912i_S Rotax 912 |
| gptkbp:performance |
Smooth operation
High power-to-weight ratio Low fuel consumption |
| gptkbp:power_output |
50 to 150 hp
|
| gptkbp:propeller |
Fixed-pitch Propeller
Variable-pitch Propeller |
| gptkbp:regulatory_compliance |
FAA regulations
EASA regulations |
| gptkbp:service |
2000 hours
|
| gptkbp:support |
Technical support
Service centers Parts availability |
| gptkbp:torque |
Varies by model
|
| gptkbp:type |
Four-stroke Engine
Two-stroke Engine |
| gptkbp:used_in |
Light Aircraft
|
| gptkbp:weight |
Varies by model
|
| gptkbp:bfsParent |
gptkb:Lycoming_Engines
|
| gptkbp:bfsLayer |
6
|