Statements (242)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:aircraft
|
| gptkbp:bfsLayer |
3
|
| gptkbp:bfsParent |
gptkb:aircraft
gptkb:Airport gptkb:Lockheed_Martin gptkb:Smithsonian_National_Air_and_Space_Museum |
| gptkbp:aircraft_operated |
gptkb:aircraft
gptkb:Company gptkb:C-5_family gptkb:Lockheed_C-5_Galaxy gptkb:C-5_B_Galaxy gptkb:Lockheed_C-5_Galaxy_family global reach fixed-wing aircraft advanced avionics in service 19.8 meters 75.3 meters strategic airlift swept wings improved fuel efficiency active service heavy transport aircraft high-wing high-wing, four-engine strategic airlift aircraft high-wing configuration large transport aircraft 68.8 meters global airlift missions 19 ft 3 in 75 ft 5 in C-5 M Super Galaxy variant approximately 380,000 lbs designed for rapid strategic airlift newer engines and systems transport large military equipment twin boom tail design |
| gptkbp:armament |
gptkb:none
|
| gptkbp:avionics |
modernized cockpit
modernized avionics suite |
| gptkbp:capacity |
up to 36 standard pallets
up to 270,000 lbs |
| gptkbp:crew |
gptkb:television_series
gptkb:6 6 personnel |
| gptkbp:decommissioned |
gptkb:none
gptkb:battle not decommissioned |
| gptkbp:design |
high-wing design
strategic airlift strategic airlift of oversized cargo |
| gptkbp:engine |
gptkb:4
four-engine General Electric C F6-80 C2 |
| gptkbp:engine_type |
gptkb:engine
GEC F6-80 C2 General Electric C F6-80 C2 |
| gptkbp:features |
large cargo hold
|
| gptkbp:first_flight |
gptkb:2006
gptkb:2009 gptkb:2010 June 30, 2006 |
| gptkbp:first_released |
gptkb:2009
gptkb:2010 |
| gptkbp:fuel_capacity |
51,000 lb
51,000 pounds 51,000 lbs |
| gptkbp:height |
19.8 meters
19.84 m 19.8 m 19 ft 3 in 19.25 m |
| https://www.w3.org/2000/01/rdf-schema#label |
C-5 M Super Galaxy
|
| gptkbp:introduced |
gptkb:1969
gptkb:2009 |
| gptkbp:landing_gear |
tricycle landing gear
triple bogey main gear tandem dual main gear |
| gptkbp:length |
75.3 meters
75.54 meters 75.54 m 247 ft 1 in 28 ft 75 ft 5 in 19.2 feet 19.25 m |
| gptkbp:manufacturer |
gptkb:Lockheed_Martin
|
| gptkbp:material |
75.54 m
|
| gptkbp:max_speed |
450 knots
518 knots 518 mph 590 mph |
| gptkbp:max_takeoff_weight |
13 ft
2,500 feet 3,500 feet 2,500 ft 840,000 pounds 381,000 lb 381,000 pounds 840,000 lb 3,500 ft 840,000 lbs |
| gptkbp:military_branch |
gptkb:aircraft
gptkb:U._S._military gptkb:C-5_M |
| gptkbp:military_technology |
gptkb:none
|
| gptkbp:mission |
humanitarian aid missions
transporting oversized cargo |
| gptkbp:modifications |
gptkb:C-5_M_Super_Galaxy_upgrade_program
engine upgrades engine upgrade |
| gptkbp:number_built |
gptkb:52
over 50 |
| gptkbp:operational_area |
gptkb:2010
humanitarian missions |
| gptkbp:operational_range |
2,400 nautical miles
2,400 mi 2,400 nautical miles with maximum payload 2,400 miles with maximum payload |
| gptkbp:operational_status |
active
|
| gptkbp:origin |
gptkb:United_States
|
| gptkbp:power_output |
4 × General Electric C F6-80 C2
|
| gptkbp:primary_user |
gptkb:aircraft
|
| gptkbp:production_years |
2006 to present
|
| gptkbp:propulsion |
22,500 lbf per engine
22,500 lbf each |
| gptkbp:range |
2,400 miles
2,400 nautical miles 2,400 nautical miles with maximum payload 2,150 miles |
| gptkbp:release_date |
gptkb:2004
gptkb:2006 |
| gptkbp:role |
airlift
strategic airlift |
| gptkbp:safety_record |
generally safe
high safety standards |
| gptkbp:seating_capacity |
12 feet
26.5 feet 13 feet 3.8 m 4.0 m 150,000 lb 130 tons 36 standard pallets 13.5 feet 28.4 m 3.7 m drive-on/drive-off capability 20 ft 4 in automated cargo handling system drive-on/drive-off nose and aft ramp nose and tail loading doors self-loading capability automated cargo loading system 34.3 m 13 ft 6 in up to 270,000 pounds up to 36 standard pallets 34,000 cubic feet up to 73 143 ft 6 in approximately 130,000 lbs approximately 280,000 lbs approximately 34,000 cubic feet nose and ramp nose and tail doors |
| gptkbp:service_ceiling |
30,000 feet
30,000 ft 35,000 ft |
| gptkbp:services |
gptkb:2009
|
| gptkbp:squadrons |
part of the USAF fleet
|
| gptkbp:stealth_features |
gptkb:none
|
| gptkbp:successor |
gptkb:C-17_Globemaster_III
gptkb:C-5_B_Galaxy |
| gptkbp:supports |
humanitarian missions
|
| gptkbp:tail_type |
T-tail
twin vertical stabilizers |
| gptkbp:upgrades |
gptkb:C-5_B_Galaxy
gptkb:C-5_M_Super_Galaxy_upgrade_program gptkb:C-5_M_Super_Galaxy_Upgrade_Program enhanced engine performance reduced maintenance costs advanced avionics improved reliability increased fuel efficiency increased payload capacity modernized cockpit enhanced safety features new engines and avionics new engines new lighting systems improved maintenance access increased operational flexibility new communication systems new software updates enhanced cargo handling systems advanced weather radar upgraded navigation systems enhanced communication links enhanced data link capabilities better emergency response systems improved fuel systems improved flight control systems new electronic warfare systems improved emergency systems improved landing gear systems revised maintenance procedures better environmental controls better anti-icing systems better crew comfort features better interoperability with other forces better noise reduction technologies better performance in hot and high conditions better structural integrity better training simulators enhanced de-icing capabilities enhanced ground support equipment compatibility enhanced mission planning tools improved cargo ramp design improved ground handling capabilities improved thrust reversers new cargo loading systems new cargo restraint systems new cargo tracking systems new hydraulic systems new operational procedures revised training programs new engines and improved fuel efficiency |
| gptkbp:variant |
gptkb:Lockheed_C-5_Galaxy
|
| gptkbp:width |
10 ft
|
| gptkbp:wing_area |
6,000 square feet
5,000 sq ft 5,700 square feet |
| gptkbp:wingspan |
68.4 meters
67.89 meters 67.89 m 222 ft 9 in 68.8 meters 68.4 m 69.0 m |