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gptkbp:instance_of
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gptkb:aircraft
|
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gptkbp:bfsLayer
|
6
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gptkbp:bfsParent
|
gptkb:Kawasaki_Aircraft_Company
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|
gptkbp:aircraft_operated
|
gptkb:aircraft
high performance
fixed-wing aircraft
advanced avionics
strategic airlift
easy access
low-wing
redundant systems
frequent upgrades
reliable transport
|
|
gptkbp:aspect_ratio
|
8.5
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|
gptkbp:avionics
|
modernized over time
|
|
gptkbp:capacity
|
up to 100 troops
|
|
gptkbp:constructed_in
|
50
|
|
gptkbp:crew
|
gptkb:3
|
|
gptkbp:decommissioned
|
gptkb:2020
|
|
gptkbp:design
|
high-wing
Kawasaki engineers
|
|
gptkbp:emergency_services
|
multiple exits
|
|
gptkbp:engine
|
2
|
|
gptkbp:engine_type
|
turbofan
|
|
gptkbp:first_flight
|
gptkb:1970
|
|
gptkbp:fuel_capacity
|
40,000 liters
|
|
gptkbp:height
|
12.0 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Kawasaki C-1
|
|
gptkbp:influenced_by
|
gptkb:Lockheed_C-130_Hercules
|
|
gptkbp:introduced
|
gptkb:1974
|
|
gptkbp:is_used_by
|
gptkb:Japan_Air_Self-Defense_Force
|
|
gptkbp:landing_gear
|
tricycle type
|
|
gptkbp:length
|
40.0 m
|
|
gptkbp:manufacturer
|
gptkb:Kawasaki_Heavy_Industries
|
|
gptkbp:material
|
4.0 m
|
|
gptkbp:max_speed
|
600 km/h
|
|
gptkbp:max_takeoff_weight
|
120,000 lb
|
|
gptkbp:mission
|
disaster relief
|
|
gptkbp:operational_area
|
gptkb:Company
gptkb:Japan
|
|
gptkbp:operational_range
|
1,500 km with maximum payload
|
|
gptkbp:primary_function
|
gptkb:public_transportation_system
|
|
gptkbp:production_years
|
1970-2020
|
|
gptkbp:range
|
2,500 km
|
|
gptkbp:retired
|
gptkb:2020
|
|
gptkbp:role
|
airlift
|
|
gptkbp:seating_capacity
|
30,000 kg
30 tons
rear ramp
roller system
|
|
gptkbp:service_ceiling
|
10,000 m
|
|
gptkbp:successor
|
gptkb:Kawasaki_C-2
|
|
gptkbp:tail_type
|
T-tail
|
|
gptkbp:variant
|
gptkb:C-1_A
gptkb:C-1_B
gptkb:C-1_C
|
|
gptkbp:wing_area
|
250 m²
|
|
gptkbp:wingspan
|
40.0 m
|