Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
gptkb:HondaJet
Cessna Citation CJ+ (proposed) |
| gptkbp:bypassRatio |
2.9:1
|
| gptkbp:certification |
gptkb:FAA_Part_33
|
| gptkbp:compressionRatio |
2-stage booster, 2-stage centrifugal
|
| gptkbp:countryOfOrigin |
gptkb:Japan
gptkb:United_States |
| gptkbp:firstFlight |
2010
|
| gptkbp:fuelType |
gptkb:Jet-A
|
| https://www.w3.org/2000/01/rdf-schema#label |
GE Honda HF120
|
| gptkbp:introduced |
2012
|
| gptkbp:length |
50 in
|
| gptkbp:mainRotorDiameter |
18.9 in
|
| gptkbp:manufacturer |
GE Honda Aero Engines
|
| gptkbp:marketedAs |
GE Honda Aero Engines
|
| gptkbp:predecessor |
Honda HF118
|
| gptkbp:thrust |
2,050 lbf
|
| gptkbp:turbineType |
2-stage low-pressure, 1-stage high-pressure
|
| gptkbp:usedIn |
light business jets
|
| gptkbp:weight |
400 lb
|
| gptkbp:bfsParent |
gptkb:HondaJet_Elite_II
|
| gptkbp:bfsLayer |
7
|