|
gptkbp:instanceOf
|
aircraft
|
|
gptkbp:aircraft
|
gptkb:Lockheed_C-130_family
gptkb:Lockheed_130
fixed-wing aircraft
twin-engine
multi-role aircraft
cantilever wing
|
|
gptkbp:armament
|
none
|
|
gptkbp:avionics
|
modernized
|
|
gptkbp:built
|
200
|
|
gptkbp:crew
|
2
required
|
|
gptkbp:decommissioned
|
1995
|
|
gptkbp:design
|
cargo transport
|
|
gptkbp:design_feature
|
high-wing configuration
|
|
gptkbp:engine
|
2
T56-A-15
|
|
gptkbp:engineConfiguration
|
Allison
|
|
gptkbp:engineType
|
turbofan
|
|
gptkbp:firstFlight
|
1960
|
|
gptkbp:fuel_capacity
|
20,000 lb
|
|
gptkbp:headlights
|
T-tail
|
|
gptkbp:height
|
8.4 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Lockheed 160C
|
|
gptkbp:inspiration
|
gptkb:United_States
|
|
gptkbp:introduced
|
1961
|
|
gptkbp:is_used_in
|
gptkb:United_States_Air_Force
|
|
gptkbp:landing_gear
|
tricycle type
|
|
gptkbp:length
|
30.2 m
|
|
gptkbp:manufacturer
|
gptkb:Lockheed_Martin
|
|
gptkbp:maximum_speed
|
600 mph
|
|
gptkbp:maxTakeoffWeight
|
70,000 lb
|
|
gptkbp:missions
|
humanitarian aid
|
|
gptkbp:modifications
|
cargo handling systems
|
|
gptkbp:nickname
|
C-130
|
|
gptkbp:operationalHistory
|
gptkb:Vietnam_War
|
|
gptkbp:operationalRange
|
2,500 miles
|
|
gptkbp:passenger_traffic
|
up to 80
45,000 lb
|
|
gptkbp:passengerCapacity
|
rear ramp
|
|
gptkbp:primaryFunction
|
airlift
|
|
gptkbp:primaryUser
|
US_Air_Force,_US_Navy
|
|
gptkbp:productionYears
|
1960-1965
|
|
gptkbp:range
|
3,000 miles
|
|
gptkbp:retired
|
1990s
|
|
gptkbp:role
|
transport aircraft
|
|
gptkbp:service_ceiling
|
30,000 ft
|
|
gptkbp:serviceType
|
1961-1995
|
|
gptkbp:successor
|
gptkb:Lockheed_C-130_Hercules
gptkb:C-130J_Super_Hercules
|
|
gptkbp:surrounding_area
|
1,500 sq ft
|
|
gptkbp:type
|
military aircraft
|
|
gptkbp:variant
|
gptkb:Lockheed_160
|
|
gptkbp:wingspan
|
28.9 m
|