Statements (25)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:turbofan_engine
|
| gptkbp:application |
aircraft propulsion
|
| gptkbp:armament |
gptkb:4
|
| gptkbp:compression_ratio |
8:1
|
| gptkbp:control_system |
gptkb:full_authority_digital_engine_control_(FADEC)
|
| gptkbp:cooling_system |
air-cooled
|
| gptkbp:diameter |
approximately 2.5 ft
|
| gptkbp:emissions_standard |
low
|
| gptkbp:engine_configuration |
twin-shaft
|
| gptkbp:first_flight |
1960s
|
| gptkbp:fuel_economy |
0.5 lb/hp/hr
|
| gptkbp:fuel_type |
gptkb:Jet_A
|
| https://www.w3.org/2000/01/rdf-schema#label |
TPE331-10 G
|
| gptkbp:length |
approximately 4.5 ft
|
| gptkbp:maintenance |
500 hours
|
| gptkbp:manufacturer |
gptkb:Honeywell
|
| gptkbp:noise_level |
low
|
| gptkbp:operational_range |
up to 25,000 ft
|
| gptkbp:power_output |
1000 shp
|
| gptkbp:propulsion |
1000 lbf
|
| gptkbp:reliability |
high
|
| gptkbp:type |
turbocharged engine
|
| gptkbp:weight |
approximately 300 lb
|
| gptkbp:bfsParent |
gptkb:Honeywell_TPE331-10_GD
|
| gptkbp:bfsLayer |
5
|