|
gptkbp:instance_of
|
gptkb:engine
|
|
gptkbp:bfsLayer
|
5
|
|
gptkbp:bfsParent
|
gptkb:AGM-158_JASSM
|
|
gptkbp:application
|
gptkb:aircraft
|
|
gptkbp:average_temperature
|
high
|
|
gptkbp:check_in_time
|
optional
|
|
gptkbp:controls
|
hydromechanical
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:design
|
gptkb:Williams_International
|
|
gptkbp:developer
|
$10 million
1950s to 1960s
|
|
gptkbp:diameter
|
3 ft 4 in
|
|
gptkbp:emissions_standard
|
Stage 3
|
|
gptkbp:engine
|
turbojet
2,000 hours
|
|
gptkbp:engine_type
|
axial
single spool
|
|
gptkbp:facilities
|
gptkb:NASA
|
|
gptkbp:features
|
modular construction
|
|
gptkbp:first_flight
|
1960s
|
|
gptkbp:fuel_capacity
|
high
moderate
|
|
gptkbp:fuel_type
|
annular
JP-4
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Williams F107-WR-100
|
|
gptkbp:introduced
|
gptkb:1960
|
|
gptkbp:invention
|
multiple
|
|
gptkbp:launch_date
|
short
|
|
gptkbp:legacy
|
influenced future designs
|
|
gptkbp:length
|
12 ft 6 in
|
|
gptkbp:maintenance
|
500 hours
|
|
gptkbp:manufacturer
|
gptkb:Williams_International
|
|
gptkbp:max_speed
|
Mach 2.2
|
|
gptkbp:noise_level
|
low
|
|
gptkbp:operational_area
|
1970s
|
|
gptkbp:origin
|
gptkb:United_States
|
|
gptkbp:performance
|
high thrust-to-weight ratio
|
|
gptkbp:propulsion
|
gptkb:battle
10,000 lbf
|
|
gptkbp:related_to
|
gptkb:F119-PW-100
|
|
gptkbp:reliability
|
high
|
|
gptkbp:research_and_development
|
ongoing
|
|
gptkbp:service_ceiling
|
40,000 ft
|
|
gptkbp:successor
|
gptkb:F119
|
|
gptkbp:type
|
gptkb:engine
|
|
gptkbp:used_in
|
gptkb:Mc_Donnell_Douglas_F-4_Phantom_II
|
|
gptkbp:weight
|
1,200 lb
|