Statements (24)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb: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:combustorType |
annular
|
| gptkbp:compressionRatio |
two-stage fan, four-stage axial, one-stage centrifugal
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
36.2 in
|
| gptkbp:family |
Honeywell HTF7000 family
|
| gptkbp:firstFlight |
1999
|
| gptkbp:length |
67.3 in
|
| gptkbp:manufacturer |
gptkb:Honeywell_Aerospace
|
| gptkbp:numberOfAxles |
2
|
| gptkbp:thrust |
6,826 lbf
|
| gptkbp:variant |
HTF7250G
HTF7350 HTF7500E |
| gptkbp:weight |
1,500 lb
|
| gptkbp:bfsParent |
gptkb:Garrett_TFE731
|
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
Honeywell HTF7000
|