Statements (26)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:jet_engine
|
| gptkbp:application |
regional aircraft
|
| gptkbp:armament |
gptkb:4
|
| gptkbp:compression_ratio |
8:1
|
| gptkbp:configuration |
free turbine
|
| gptkbp:control_system |
gptkb:full_authority_digital_engine_control_(FADEC)
|
| gptkbp:cooling_system |
air-cooled
|
| gptkbp:diameter |
0.9 m
|
| gptkbp:emissions_standard |
ICAO Chapter 4
|
| gptkbp:engine |
Brayton cycle
|
| gptkbp:engine_configuration |
twin-shaft
|
| gptkbp:first_flight |
gptkb:1960
|
| gptkbp:fuel_economy |
0.5 kg/hp/h
|
| gptkbp:fuel_type |
gptkb:Jet_A-1
|
| https://www.w3.org/2000/01/rdf-schema#label |
Walter M601 D
|
| gptkbp:length |
1.5 m
|
| gptkbp:maintenance |
1000 hours
|
| gptkbp:manufacturer |
gptkb:Walter_Engines
|
| gptkbp:power_output |
600 hp
|
| gptkbp:propulsion |
1200 lbf
|
| gptkbp:reliability |
high
|
| gptkbp:type |
gptkb:turbofan_engine
|
| gptkbp:used_in |
Let L-410 Turbolet
|
| gptkbp:weight |
150 kg
|
| gptkbp:bfsParent |
gptkb:Walter_M601
|
| gptkbp:bfsLayer |
7
|