Honeywell F124-GA-100 turbofan
GPTKB entity
Statements (20)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
gptkb:trainer_aircraft
|
| gptkbp:bypassRatio |
0.34:1
|
| gptkbp:combustorType |
annular
|
| gptkbp:compressionRatio |
2-stage fan, 5-stage LP compressor, 4-stage HP compressor
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
0.89 m
|
| gptkbp:family |
gptkb:Honeywell_F124
|
| gptkbp:firstFlight |
1991
|
| gptkbp:hasTower |
single-stage HP, single-stage LP
|
| https://www.w3.org/2000/01/rdf-schema#label |
Honeywell F124-GA-100 turbofan
|
| gptkbp:length |
2.3 m
|
| gptkbp:manufacturer |
gptkb:Honeywell_Aerospace
|
| gptkbp:thrust |
28 kN
|
| gptkbp:type |
non-afterburning turbofan
|
| gptkbp:usedIn |
gptkb:Aero_L-159_Alca
gptkb:Aermacchi_M-346 |
| gptkbp:weight |
620 kg
|
| gptkbp:bfsParent |
gptkb:Boeing_X-45
|
| gptkbp:bfsLayer |
6
|