|
gptkbp:instance_of
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gptkb:engine
|
|
gptkbp:bfsLayer
|
4
|
|
gptkbp:bfsParent
|
gptkb:General_Electric_F110
|
|
gptkbp:aircraft_operated
|
gptkb:F-16
gptkb:F-15
|
|
gptkbp:controls
|
digital electronic control
|
|
gptkbp:diameter
|
3 ft 4 in
|
|
gptkbp:engine
|
gptkb:F414-GE-400
gptkb:F119-PW-100
gptkb:F135-PW-100
gptkb:F120-GE-100
F404-GE-400
twin-spool
F118-GE-100
|
|
gptkbp:engine_type
|
axial
single-stage high-pressure turbine
|
|
gptkbp:first_flight
|
gptkb:1986
|
|
gptkbp:fuel_capacity
|
0.8 lb/lbf/hr
|
|
gptkbp:fuel_type
|
gptkb:JP-8
annular
|
|
gptkbp:has_programs
|
F-15 and F-16 engine program
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
F110-GE-100
|
|
gptkbp:length
|
16 ft 8 in
|
|
gptkbp:manufacturer
|
gptkb:General_Electric
|
|
gptkbp:military_branch
|
gptkb:aircraft
gptkb:battle
|
|
gptkbp:notable_feature
|
modular design
advanced materials
reliable performance
high thrust-to-weight ratio
low maintenance requirements
|
|
gptkbp:operational_area
|
gptkb:1990
|
|
gptkbp:operational_range
|
2,000 miles
|
|
gptkbp:propulsion
|
29,000 lbf
|
|
gptkbp:service_ceiling
|
50,000 ft
|
|
gptkbp:successor
|
gptkb:F119-PW-100
|
|
gptkbp:type
|
afterburning turbofan
|
|
gptkbp:used_in
|
gptkb:F-15_Eagle
gptkb:star
|
|
gptkbp:weight
|
3,000 lb
|