Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
gptkb:Gulfstream_G280
gptkb:Bombardier_Challenger_300 gptkb:Embraer_Legacy_450 gptkb:Embraer_Legacy_500 |
| gptkbp:bypassRatio |
4.2:1
|
| gptkbp:certification |
gptkb:FAA
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
28.9 in
|
| gptkbp:family |
gptkb:HTF7000_series
|
| gptkbp:firstFlight |
2002
|
| gptkbp:fuelType |
gptkb:Jet-A
|
| gptkbp:hasConcept |
two-spool
|
| https://www.w3.org/2000/01/rdf-schema#label |
Honeywell HTF7000 engine
|
| gptkbp:length |
67.3 in
|
| gptkbp:manufacturer |
gptkb:Honeywell_Aerospace
|
| gptkbp:market |
business jet
|
| gptkbp:numberOfStages |
2-stage high-pressure, 2-stage low-pressure
3-stage fan, 4-stage axial, 1-stage centrifugal |
| gptkbp:thrust |
6,826 lbf
|
| gptkbp:weight |
1,500 lb
|
| gptkbp:bfsParent |
gptkb:Honeywell_Aerospace
|
| gptkbp:bfsLayer |
6
|