Statements (22)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
turboshaft engine
|
| gptkbp:application |
military aviation
|
| gptkbp:controls |
gptkb:full_authority_digital_engine_control_(FADEC)
|
| gptkbp:coolingSystem |
air-cooled
|
| gptkbp:emissionsStandard |
meets current standards
|
| gptkbp:engineType |
axial compressor
single-stage turbine |
| gptkbp:firstRace |
2020
|
| gptkbp:fuelType |
Jet A
annular combustor |
| https://www.w3.org/2000/01/rdf-schema#label |
General Electric T901
|
| gptkbp:is_designed_to |
helicopters
|
| gptkbp:is_used_in |
Future Vertical Lift program
|
| gptkbp:maintenance |
extended maintenance intervals
|
| gptkbp:manufacturer |
gptkb:General_Electric
|
| gptkbp:noise_level |
yes
|
| gptkbp:operationalRange |
wide range of altitudes
|
| gptkbp:powerOutput |
up to 2,000 shp
|
| gptkbp:propulsion |
4:1
|
| gptkbp:successor |
T700 engine
|
| gptkbp:training |
T901_program
|
| gptkbp:weight |
approximately 500 lb
|